advances in the acoustics of flow ducts and mufflers
2023 年湍流与噪声和 CFD 方法暑期高级讲习班 会议手册说明书
2023年湍流与噪声和CFD方法暑期高级讲习班2023 Advanced Summer Program on Turbulence,Noise and CFD Methods会议手册时间:2023年7月28至8月5日地点:香港科技大学主办单位:中国空气动力学会承办单位:香港科技大学(HKUST)上海大学南方科技大学复旦大学中国空气动力学会CFD专委会中国空气动力学会低跨超专委会上海市应用数学和力学研究所上海市力学信息学前沿科学基地上海市能源工程力学重点实验室粤港澳数据驱动下的流体力学与工程应用联合实验室中国航空学会航空声学分会协办单位:《空气动力学学报》《实验流体力学》《Advances in Aerodynamics》二零二三年七月二十六日2023年湍流与噪声和CFD方法暑期高级讲习班为了促进流体力学与空气动力学的发展、推动学术交流与合作、培育培养优秀人才,助力解决流体力学与空气动力学等相关领域“卡脖子”技术,经中国空气动力学会批准,2023年湍流与噪声和CFD 方法暑期高级讲习班将于2023年7月28日至8月5日在香港科技大学(HKUST)举行。
会议邀请内地与香港地区在湍流、噪声和CFD方法等方面的专家学者、青年学者为讲习班授课。
现诚邀内地与港澳台地区研究生、工程师、相关领域专家学者以及高年级本科生参会。
本次讲习班由中国空气动力学会主办,香港科技大学(HKUST)、上海大学、南方科技大学、复旦大学、中国空气动力学会CFD专委会、中国空气动力学会低跨超专委会、上海市应用数学和力学研究所、上海市力学信息学前沿科学基地、上海市能源工程力学重点实验室、粤港澳数据驱动下的流体力学与工程应用联合实验室等单位承办。
本次讲习班采用线上线下同时进行的方式,其中线上使用腾讯会议App进行直播,会议号码:964-8147-9182,也可直接扫描下面的二维码参会:2023年湍流与噪声和CFD方法暑期高级讲习班专家报告日程安排报告安排以专家自选日程排列,不分先后次序,后续如有变动以最终表格为准。
基于Virtual.Lab Acoustics的管道壁面声阻抗优化分析
Optimization and Analysis of Acoustic Impedance of Duct Wall Based on b Acoustics
Weiguang Zheng, Peng Xu, Zeyu Lin, Rongjiang Tang
School of Mechanical and Electrical Engineering, Guilin University of Electronic Technology, Guilin Guangxi
∫ [ N ] dΩ
其中 [ K ] 为声学刚度矩阵, [C ] 为声学阻尼矩阵, [ F ] 为声学激励。 在得到形函数的情况下,求解式(11)就可以得到节点处的声压。 为验证本文方法的准确性,采用文献[2]同样的模型。管道截面形状为正方形,边长取 0.066 m,管长 度取 1.2 m。管道内壁边存在两种边界条件,即刚性壁面条件与阻抗边界条件。在管道入口处施加单位速 度边界条件,出口施加无反射边界属性。管道壁面为刚性,声衬处采用法向阻抗边界条件。管道采用六 面体声学网格,网格大小为 6 mm,计算频率区间取 500 Hz 到 1500 Hz,网格单元数量为 2.42 万(图 2)。
法向阻抗边界条件 Ω z
(8)
p ∂p = − jρ0ω Zn ∂n
则
(9)
Ω = Ω r + Ωv + Ω z
(10)
和 p 具有相同的形函数,将式(4)与式(7)至式(10)代入式(6)中,经整理可得 假设 p
2 − jρ0ωun ∫ [ K ] + jρ0ω Z [C ] − k0 [C ] [ pi ] =
3.1. 声学仿真优化计算
模型的边界条件与优化参数的设置直接影响到声学仿真优化的准确性,本文采用 Tester [6]研究所得 的经验公式算出初始阻抗值,并在此基础上进行优化。以下表 1 与表 2 分别对应管内无流与有稳定切向 流两种情况下, 壁面最优声阻抗 Z (Z = Zo/ρ0c0, Zo 为最优阻抗值, ρ0c0 为空气特性阻抗, 本文取 416.5 kg/m2/s) 和传递损失,并将最优阻抗数值解与文献[5]的优化结果进行了对比(图 3)。
所有声学测试标准 Acoustics-Application
Test Method Designation Short Title______08/P01ASTM C367Strength properties of prefabricated architecturalacoustical tile or lay-in ceiling panels______08/P04ASTM C522Airflow resistance of acoustical materials______08/P09ASTM E756Measuring vibration-damping properties of materials ______08/P55SAE J1637Laboratory measurement of the composite vibrationdamping properties of materials on a supportingsteel bar______08/P61AAMA 1801Acoustical rating of windows, doors, and glazed wallsystems ______08/P02ASTM C384Impedance and absorption of acoustical materials bythe impedance tube method______08/P03ASTM C423Sound absorption and sound absorption coefficientsby the reverberation room method______08/P35ASTM E1050Impedance and absorption of acoustical materialsusing a tube, two microphones, and a digitalfrequency analysis system______08/P44ISO 354Acoustics - Measurement of sound absorption in areverberation room Instruction: Check each test method for which you are requesting accreditation.Note: Accreditation is limited to the frequency range for which the test room has beenqualified.ACOUSTICAL TESTING SERVICESTEST METHOD SELECTION LISTNVLAP TestMethod Code MATERIAL PROPERTIES SOUND ABSORPTION______08/P72AS ISO 354Acoustics - Measurement of sound absorption in areverberation room______08/P98NFPA 1981 (Sec. 3.3.49, 7.10, 7.17, 8.10, and 8.15)Open-Circuit Self-Contained Breathing Apparatus(SCBA) for Emergency Services______08/P31ASTM E336Measurement of airborne sound insulation inbuildings______08/P37ASTM E966Guide for field measurement of airborne soundinsulation of building facades and facade elements ______08/P06ASTM E90Laboratory measurement of airborne soundtransmission loss of building partitions______08/P96BS EN ISO 10140-2Acoustics - Laboratory measurement of soundinsulation of building elements - Measurement ofairborne sound insulation ______08/P08ASTM E596Laboratory measurement of noise reduction of sound-isolating enclosures______08/P33ASTM E1111Measuring the interzone attenuation of ceilingsystems______08/P34ASTM E1414Airborne sound attenuation between rooms sharinga common ceiling plenum______08/P36ASTM E477Measuring acoustical and airflow performance ofduct liner materials and prefabricated silencers______08/P49AMA-1-II-67Ceiling sound transmission test by two-room method FieldLaboratory - Set 1Laboratory - Set 2Device SpecificSOUND TRANSMISSION - AIRBORNE______08/P54SAE J1400Laboratory measurement of the airborne soundbarrier performance of automotive materials andassemblies______08/P58ASTM E1222Laboratory measurement of the insertion loss of pipelagging systems______08/P71AS/NZS 2499Measurements of sound insulation in buildings and ofbuilding elements - Laboratory measurement ofroom-to-room airborne sound insulation of asuspended ceiling with a plenum above it______08/P92ISO 7235Acoustics - Laboratory measurement procedures forducted silencers and air-terminal units - Insertionloss, flow noise and total pressure loss______08/P93ISO 11691Acoustics - Measurement of insertion loss of ductedsilencers without flow - Laboratory survey method______08/P99ANSI S3.1Maximum permissible ambient noise levels foraudiometric test rooms ______08/P32ASTM E1007Field measurement of tapping machine impact soundtransmission through floor-ceiling assemblies andassociated support structures______08/P94ASTM E1124Field measurement of sound power level by the two-surface method______08/P95ASTM E1574Measurement of sound in residential spaces ______08/P07ASTM E492Laboratory measurement of impact soundtransmission through floor-ceiling assemblies usingthe tapping machine______08/P59ASTM E2179Laboratory measurement of the effectiveness offloor coverings in reducing impact soundtransmission through concrete floors SOUND TRANSMISSION - STRUCTURE BORNEFieldLaboratory______08/P76ISO 10848-2Acoustics - Laboratory measurement of the flankingtransmission of airborne and impact sound betweenadjoining rooms - Part 2: Application to lightelements when the junction has a small influence______08/P11ISO 3744Acoustics - Determination of sound power levels andsound energy levels of noise sources using soundpressure - Engineering methods for an essentiallyfree field over a reflecting plane______08/P21ISO 3745Acoustics - Determination of sound power levels andsound energy levels of noise sources using soundpressure - Precision methods for anechoic rooms andhemi-anechoic rooms______08/P46ISO 3741Acoustics - Determination of sound power levels andsound energy levels of noise sources using soundpressure - Precision methods for reverberation testrooms______08/P60ANSI S12.51Determination of sound power levels of noisesources using sound pressure - precision method forreverberation rooms______08/P62ANSI S12.54Determination of sound power levels of noisesources using sound pressure - Engineering methodin an essentially free field over a reflecting plane______08/P63ANSI S1.10Method for calibration of microphones______08/P79ANSI S12.55Determination of sound power levels of noisesources using sound pressure - Precision methods foranechoic and hemi-anechoic rooms ______08/P24ANSI S12.10Measurement and designation of noise emitted bycomputer and business equipmentSOUND POWERGenericMachine Specific______08/P38ANSI S12.11Measurement of noise emitted by small air-movingdevices______08/P39ANSI S12.5Requirements for the performance and calibration ofreference sound sources______08/P40ISO 9296Acoustics - Declared noise emission values ofcomputer and business equipment______08/P41ECMA 74Measurement of airborne noise emitted byinformation technology and telecommunicationequipment______08/P48ISO 7779Acoustics - Measurement of airborne noise emittedby information technology and telecommunicationsequipment______08/P51ISO 6926Acoustics - Requirements for the performance andcalibration of reference sound sources used for thedetermination of sound power levels______08/P52ISO 3822Laboratory tests on noise emission from appliancesand equipment used in water supply installations______08/P53SAE J1477Measurement of interior sound levels of lightvehicles______08/P65ISO 11201Noise emitted by machinery and equipment -Determination of emission sound pressure levels at awork station and at other specified positions in anessentially free field over a reflecting plane withnegligible environmental corrections______08/P67IEC 60704-1Household and similar electrical appliances - Testcode for the determination of airborne acousticalnoise emitted by household and similar electricalappliances - Part 1: General requirements______08/P68IEC 60704-2-3Household and similar electrical appliances - Testcode for the determination of airborne acousticalnoise - Part 2-3: Particular requirements fordishwashers______08/P69ECMA 109Declared noise emission values of informationtechnology and telecommunications equipment______08/P73ISO 10302Acoustics - Measurement of airborne noise emittedand structure-borne vibration induced by small air-moving devices______08/P75IEC 60704-2-4Household and similar electrical appliances - Testcode for the determination of airborne acousticalnoise - Part 2-4: Particular requirements for washingmachines and extractors______08/P77IEC 60704-2-6Household and similar electrical appliances - Testcode for the determination of airborne acousticalnoise - Part 2-6: Particular requirements for tumble-dryers______08/P78ANSI S12.15Portable electric power tools, stationary and fixedelectric power tools, and gardening appliances -Measurement of sound emitted______08/P80IEC 60704-2-14Household and similar electrical appliances - Testcode for the determination of airborne acousticalnoise - Part 2-14: Particular requirements forrefrigerators, frozen-food storage cabinets and foodfreezers______08/P90ISO 3747Acoustics - Determination of sound power levels andsound energy levels of noise sources using soundpressure - Engineering/survey methods for use in situin a reverberant environment______08/P26ANSI S3.19 (ANSI S3.19-1974)Measurement of real-ear protection of hearing protectors and physical attenuation of earmuffs______08/P27ANSI S12.6Methods for measuring the real-ear attenuation ofhearing protectors______08/P66AS/NZS 1270Acoustics - Hearing protectorsHEARING PROTECTORS______08/P81ANSI S12.42Methods for measurement of insertion loss ofhearing protection devices in continuous orimpulsive noise using microphone-in-real-ear oracoustics test fixture procedures______08/P82BS EN 352-1Hearing protectors - Safety requirements and testing -Ear-muffs______08/P83BS EN 352-2Hearing protectors - Safety requirements and testing -Ear-plugs______08/P84BS EN 352-3Hearing protectors - Safety requirements and testing -Ear-muffs attached to an industrial safety helmet______08/P85BS EN 352-4Hearing protectors - Safety requirements and testing -Level-dependent ear-muffs______08/P86BS EN 352-5Hearing protectors - Safety requirements and testing -Active noise reduction ear-muffs______08/P87BS EN 352-6Hearing protectors - Safety requirements and testing -Ear-muffs with electrical audio input______08/P88BS EN 352-7Hearing protectors - Safety requirements and testing -Level-dependent ear-plugs______08/P89BS EN 352-8Hearing protectors - Safety requirements and testing -Entertainment audio ear-muffsSTANDARD PRACTICES______08/P43ASTM E1425Standard practice for determining the acousticalperformance of exterior windows and doors______08/P64ASTM E1816Standard practice for ultrasonic examinations usingelectromagnetic acoustic transducer (EMAT)techniques______08/P70ASTM E795Standard practice for mounting test specimensduring sound absorption tests______08/P91MIL-STD-1474D Department of Defense design criteria standard -Noise limits______08/P97ASTM E2235-04 Determination of decay rates for use in soundinsulation test methodsOTHERPlease list additional test methods for which you seek accreditation.。
None
THIS MAY COMPRISE THE CONFIDENTIALITY OF THE INFORMATION.PI/PD Name:Gender:Male FemaleEthnicity: (Choose one response)Hispanic or Latino Not Hispanic or LatinoRace:(Select one or more)American Indian or Alaska NativeAsianBlack or African AmericanNative Hawaiian or Other Pacific Islander WhiteDisability Status: (Select one or more)Hearing ImpairmentVisual ImpairmentMobility/Orthopedic Impairment OtherNoneCitizenship: (Choose one)U.S. Citizen Permanent Resident Other non-U.S. Citizen Check here if you do not wish to provide any or all of the above information (excluding PI/PD name):REQUIRED: Check here if you are currently serving (or have previously served) as a PI, co-PI or PD on any federally funded projectEthnicity Definition:Hispanic or Latino. A person of Mexican, Puerto Rican, Cuban, South or Central American, or other Spanish culture or origin, regardlessof race.Race Definitions:American Indian or Alaska Native. 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A person having origins in any of the original peoples of Europe, the Middle East, or North Africa.WHY THIS INFORMATION IS BEING REQUESTED:The Federal Government has a continuing commitment to monitor the operation of its review and award processes to identify and address any inequities based on gender, race, ethnicity, or disability of its proposed PIs/PDs. To gather information needed for this important tasks, the proposer should submit a single copy of this form for each identified PI/PD with each proposal. Submission of the requested information is voluntary and is not a precondition of award. However, information not submitted will seriously undermine the statistical validity, and therefore the usefulness, of information recieved from others. Any individual not wishing to submit some or all the information should check the box provided for this purpose. (The exceptions are the PI/PD name and the information about prior Federal support, the last question above.)Collection of this information is authorized by the NSF Act of 1950, as amended, 42 U.S.C. 1861, et seq. Demographic data allows NSF to gauge whether our programs and other opportunities in science and technology are fairly reaching and benefiting everyone regardless of demographic category; to ensure that those in under-represendted groups have the same knowledge of and access to programs and other research and educational oppurtunities; and to assess involvement of international investigators in work supported by NSF. The information may be disclosed to government contractors, experts, volunteers and researchers to complete assigned work; and to other government agencies in order to coordinate and assess programs. The information may be added to the Reviewer file and used to select potential Mohammed Y HussainiTHIS MAY COMPRISE THE CONFIDENTIALITY OF THE INFORMATION.PI/PD Name:Gender:Male FemaleEthnicity: (Choose one response)Hispanic or Latino Not Hispanic or LatinoRace:(Select one or more)American Indian or Alaska NativeAsianBlack or African AmericanNative Hawaiian or Other Pacific Islander WhiteDisability Status: (Select one or more)Hearing ImpairmentVisual ImpairmentMobility/Orthopedic Impairment OtherNoneCitizenship: (Choose one)U.S. Citizen Permanent Resident Other non-U.S. Citizen Check here if you do not wish to provide any or all of the above information (excluding PI/PD name):REQUIRED: Check here if you are currently serving (or have previously served) as a PI, co-PI or PD on any federally funded projectEthnicity Definition:Hispanic or Latino. A person of Mexican, Puerto Rican, Cuban, South or Central American, or other Spanish culture or origin, regardlessof race.Race Definitions:American Indian or Alaska Native. A person having origins in any of the original peoples of North and South America (including Central America), and who maintains tribal affiliation or community attachment.Asian. A person having origins in any of the original peoples of the Far East, Southeast Asia, or the Indian subcontinent including, for example, Cambodia, China, India, Japan, Korea, Malaysia, Pakistan, the Philippine Islands, Thailand, and Vietnam.Black or African American. A person having origins in any of the black racial groups of Africa.Native Hawaiian or Other Pacific Islander. A person having origins in any of the original peoples of Hawaii, Guam, Samoa,or other Pacific Islands.White. A person having origins in any of the original peoples of Europe, the Middle East, or North Africa.WHY THIS INFORMATION IS BEING REQUESTED:The Federal Government has a continuing commitment to monitor the operation of its review and award processes to identify and address any inequities based on gender, race, ethnicity, or disability of its proposed PIs/PDs. To gather information needed for this important tasks, the proposer should submit a single copy of this form for each identified PI/PD with each proposal. Submission of the requested information is voluntary and is not a precondition of award. However, information not submitted will seriously undermine the statistical validity, and therefore the usefulness, of information recieved from others. Any individual not wishing to submit some or all the information should check the box provided for this purpose. (The exceptions are the PI/PD name and the information about prior Federal support, the last question above.)Collection of this information is authorized by the NSF Act of 1950, as amended, 42 U.S.C. 1861, et seq. Demographic data allows NSF to gauge whether our programs and other opportunities in science and technology are fairly reaching and benefiting everyone regardless of demographic category; to ensure that those in under-represendted groups have the same knowledge of and access to programs and other research and educational oppurtunities; and to assess involvement of international investigators in work supported by NSF. The information may be disclosed to government contractors, experts, volunteers and researchers to complete assigned work; and to other government agencies in order to coordinate and assess programs. The information may be added to the Reviewer file and used to select potential Geoffrey C FoxCOVER SHEET FOR PROPOSAL TO THE NATIONAL SCIENCE FOUNDATION FOR NSF USE ONLY NSF PROPOSAL NUMBER DATE RECEIVED NUMBER OF COPIES DIVISION ASSIGNED FUND CODE DUNS#(Data Universal Numbering System)FILE LOCATION FOR CONSIDERATION BY NSF ORGANIZATION UNIT(S) (Indicate the most specific unit known, i.e. program, division, etc.)PROGRAM ANNOUNCEMENT/SOLICITATION NO./CLOSING DATE /if not in response to a program announcement/solicitation enter NSF 00-2EMPLOYER IDENTIFICATION NUMBER (EIN) ORTAXPAYER IDENTIFICATION NUMBER (TIN)SHOW PREVIOUS AWARD NO. IF THIS IS A RENEWALAN ACCOMPLISHMENT-BASED RENEWAL IS THIS PROPOSAL BEING SUBMITTED TO ANOTHER FEDERAL AGENCY? 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RESEARCH (SGER) (GPG II.D.12)GROUP PROPOSAL (GPG II.D.12)VERTEBRATE ANIMALS (GPG II.D.12) IACUC App. Date HUMAN SUBJECTS (GPG II.D.12)Exemption Subsection or IRB App. Date INTERNATIONAL COOPERATIVE ACTIVITIES: COUNTRY/COUNTRIESFACILITATION FOR SCIENTISTS/ENGINEERS WITH DISABILITIES (GPG V.G.)RESEARCH OPPORTUNITY AWARD (GPG V.H)PI/PD DEPARTMENTPI/PD POSTAL ADDRESS PI/PD FAX NUMBER NAMES (TYPED)High DegreeYr of Degree Telephone Number Electronic Mail Address PI/PD NAME CO-PI/PD CO-PI/PDCO-PI/PDCO-PI/PDNSF Form 1207 (10/98)Page 1 of 20080220DIRECT FOR COMPUTER & INFO SCIE & ENGINRNSF-00501/25/00596001138Florida State University0014894000Florida State University Tallahassee, FL. 32306Research and Education Infrastructure Proposal1,950,000 6007/31/00850-645-0300School of CSIT 150 Dirac Science Center Library Tallahassee, FL 323064120United States Mohammed Y HussainiPh.D.1970850-645-0305myh@ Geoffrey C FoxPh.D.1967315-443-2163gcf@ 790877419CERTIFICATION PAGE Certification for Principal Investigators and Co-Principal Investigators:I certify to the best of my knowledge that:(1) the statements herein (excluding scientific hypotheses and scientific opinions) are true and complete, and(2) the text and graphics herein as well as any accompanying publications or other documents, unless otherwise indicated, are the original work of thesignatories or individuals working under their supervision. I agree to accept responsibility for the scientific conduct of the project and to provide therequired progress reports if an award is made as a result of this application.I understand that the willful provision of false information or concealing a material fact in this proposal or any other communication submitted to NSF is acriminal offense (U.S.Code, Title 18, Section 1001).Name (Typed)Signature Social Security No.*Date PI/PD Co-PI/PDCo-PI/PDCo-PI/PDCo-PI/PDCertification for Authorized Organizational Representative or Individual Applicant:By signing and submitting this proposal, the individual applicant or the authorized official of the applicant institution is: (1) certifying thatstatements made herein are true and complete to the best of his/her knowledge; and (2) agreeing to accept the obligation to comply with NSFaward terms and conditions if an award is made as a result of this application. 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Yes No Certification Regarding LobbyingThis certification is required for an award of a Federal contract, grant, or cooperative agreement exceeding $100,000 and for an award of a Federal loan ora commitment providing for the United States to insure or guarantee a loan exceeding $150,000.Certification for Contracts, Grants, Loans and Cooperative AgreementsThe undersigned certifies, to the best of his or her knowledge and belief, that:(1) No federal appropriated funds have been paid or will be paid, by or on behalf of the undersigned, to any person for influencing or attempting to influencean officer or employee of any agency, a Member of Congress, an officer or employee of Congress, or an employee of a Member of Congress in connectionwith the awarding of any federal contract, the making of any Federal grant, the making of any Federal loan, the entering into of any cooperative agreement,and the extension, continuation, renewal, amendment, or modification of any Federal contract, grant, loan, or cooperative agreement.(2) If any funds other than Federal appropriated funds have been paid or will be paid to any person for influencing or attempting to influence an officer oremployee of any agency, a Member of Congress, an officer or employee of Congress, or an employee of a Member of Congress in connection with thisFederal contract, grant, loan, or cooperative agreement, the undersigned shall complete and submit Standard Form-LLL, ‘‘Disclosure Form to ReportLobbying,’’ in accordance with its instructions.(3) The undersigned shall require that the language of this certification be included in the award documents for all subawards at all tiers includingsubcontracts, subgrants, and contracts under grants, loans, and cooperative agreements and that all subrecipients shall certify and disclose accordingly.This certification is a material representation of fact upon which reliance was placed when this transaction was made or entered into. Submission of thiscertification is a prerequisite for making or entering into this transaction imposed by section 1352, title 31, U.S. Code. Any person who fails to file therequired certification shall be subject to a civil penalty of not less than $10,000 and not more than $100,000 for each such failure.AUTHORIZED ORGANIZATIONAL REPRESENTATIVE SIGNATURE DATENAME/TITLE (TYPED)TELEPHONE NUMBER ELECTRONIC MAIL ADDRESS FAX NUMBERMohammed Y HussainiSSNs are confidential and are not displayed *ON FASTLANE SUBMISSIONS*Geoffrey C FoxRaymond E. Bye, Jr.,Interim VP Rsrc01/27/00850-644-5260nsfaward@ 850-644-1464TABLE OF CONTENTS For font size and page formatting specifications, see GPG section II.C.Section Total No. of Page No.*Pages in Section (Optional)*Cover Sheet (NSF Form 1207 - Submit Page 2 with original proposal only)AProject Summary (not to exceed 1 page) BTable of Contents (NSF Form 1359) C Project Description (including Results from PriorNSF Support) (not to exceed 15 pages) (Exceed only if allowed by aspecific program announcement/solicitation or if approved inadvance by the appropriate NSF Assistant Director or designee) DReferences Cited EBiographical Sketches (Not to exceed 2 pages each) F Budget(NSF Form 1030, including up to 3 pages of budget justification) GCurrent and Pending Support (NSF Form 1239) HFacilities, Equipment and Other Resources (NSF Form 1363) ISpecial Information/Supplementary Documentation J Appendix (List below. )(Include only if allowed by a specific program announcement/solicitation or if approved in advance by the appropriate NSFAssistant Director or designee)Appendix Items:*Proposers may select any numbering mechanism for the proposal, however, the entire proposal must be plete both columns only if the proposal is numbered consecutively.NSF Form 1359 (10/98) 15115623121300Research Description1IntroductionWe will address problems from grand challenge applications that require high-performance algo-rithm/architecture combinations and supporting software infrastructure.We will develop state-of-the-art numerical algorithms for simulations in such areas as climate dynamics,composite man-ufacturing processes,turbulence and acoustics and geodynamics.Well-conditioned,high-order methods will be employed to discretize spatial and temporal operators to maximize accuracy per degree of freedom.The solver engine will be an architecturally driven,solution-adaptive,domain decomposition-based iteration.High performance implementations on a distributed memory machine or a scalable shared mem-ory machine will be analyzed and their limits identified relative to the interaction of the architecture and system software with the simulation algorithm.Scalability will come from keeping commu-nication complexity of lower order than computational complexity,and maintaining load balance despite adaptive resolution and inhomogeneous source-term activity,by means of both dynamic local and periodic global balancing.We will build integrated environments for simulation and visualization which are both portable and robust in the hands of users who are not experts in numerics but in the physical processes.Its symbolic processing component will provide a natural language for the manipulation of differential equations,numerical algorithms,input/output data,processes and associated visualization.It will further include symbolic processing necessary to support multiple structured/unstructured subdomains and interfacial boundary conditions associated with higher-order discretizations.Other capabilities will include powerful collaboration techniques,customizability for each user with an architecture that will allow the environment to be used in both research and education.Our work in programming environments will focus on the development of parallel and dis-tributed programs built around Java as a core scientific language with high performance.We have proposed an elegant expression of data parallelism which can be implemented with either threads or classic message passing(MPI).This research should lead to more productive scientific program-ming environments that can both express complex scalable algorithms and link to the rich Internet infrastructure.Upon completion,this work will have significantly advanced the state of the art in core areas of CISE interest–advanced parallel algorithms,high-performance computing,scientific visualization, programming and problem-solving environments and tools.Apart from enabling the solution of the Grand Challenge problems discussed in the Multidisciplinary Applications section,this core technology will create many software solutions that are transferable to other partial-differential-equations-based applications of interest to the nation.2Core Technology2.1High-Order Numerical Methods for Parallel ArchitecturesInvestigators:G.Erlebacher,K.Gallivan,M.Hussaini, D.Keyes,M.Sussman,S. Woodruff.The primary application areas that will benefit from the requested infrastructure share a basis influid mechanics,and,from a mathematical standpoint,a basis in partial differentialevolution equations.As such,the numerical difficulties encountered in these applications and the algorithms developed to surmount these difficulties have important similarities.Below are discussed aspects of spatial discretization,grids and iteration strategies which are being addressed by innovative new algorithms in the applications areas.In all the applications,efforts are being made to transfer algorithm technology betweenfields and to develop algorithms with the target architecture in mind.Discretization Techniques and Algorithm Development.The equations describing theflow in climate dynamics or in liquid composite molding process will be spatially discretized by spectral discretization techniques(Canuto et al.1987).In this way,maximum resolving power per grid point will be achieved and memory requirements will be reduced.The increased accuracy per grid point more than compensates for the increased cost per iteration.High-order spectral methods are adaptable to complex geometries through spectral-element formulations(Kopriva1998),where,likefinite-element methods,the solution domain is divided into elements that accommodate the arbitrarily complex geometry.The solution within the elements is then approximated spectrally to the desired accuracy.The discontinuous spectral Galerkin or spectral collocation formulation(Lesaint and Raviart1974)is currently being developed by the bining high accuracy with the ability to handle material discontinuities(Kopriva et al.1999)and a strong potential for effective parallelization(Biswas et al.1994),this technique has been effectively applied toflow problems(Warburton et al.1997,Rasetarinera et al.1998,1999) and electromagnetic scattering problems(Kopriva et al.1999).This technique will be coupled with the Level Set procedures(Sussman1999)that are being investigated for tracking solution discontinuities such as shocks and other singular surfaces(Hussaini and Sussman2000)to track weather fronts or the air-resin interfaces.Consistent with the numerical methodology,we propose to construct surrogate models based on the proper orthogonal decomposition(POD)or the singular value decomposition(SVD)of data obtained from high-resolution numerical simulations of the original model.Basis functions are gen-erated based on a collection offlow snapshots via the singular value decomposition of the snapshots (Sirovich1987).These snapshots can cover several complete simulations,or several snapshots in time from a single simulation.We will combine the POD/SVD viewpoint with the Krylov subspace theory of surrogate models(Grimme1997)to derive highly efficient parallel surrogate production algorithms and demonstrate their effective use.The proposed numerical methodology enables effi-cient construction of such surrogate models(with a priori error estimates)by employing the tangent linear operator and its adjoint.New implicit time-advancement algorithms permitting computations for unsteady problems to proceed with efficient time steps will be developed.Newton-Krylov techniques(such as the Arnoldi method(Saad1981)and GMRES(Saad and Schultz1986))and Krylov-Schwartz preconditioners (such as the additive-Schwartz techniques that are natural with domain-decomposition paralleliza-tion strategies(Keyes1999))at the focus of the proposed research will accomplish these goals both through the efficiency of the algorithms themselves and the effectiveness with which they may be parallelized.EN-like methods(Yang1995,Yang and Gallivan1995)are a new class of methods which subsume methods like GMRES and allow adaptation of the form of the algorithm to a partic-ular computational platform,including parallel platforms.These methods have been demonstrated to be competitive and often superior to methods such as GMRES.2.2VisualizationInvestigators:D.Banks,G.Erlebacher,M.Hussaini,B.Jobard,S.Woodruff.Rapid advances in computer performance have produced an explosion of large scale numerical simulations to solve grand challenge problems in many areas of science and engineering.These simulations are generally governed by a system of nonlinear,time-dependent partial differential equations.They often produce extremely large datasets which must be post-processed to extract relevant information necessary both to test current theoretical concepts and to develop new models.Examples of large-scale simulations are provided by the applications-driven research in this proposal:coupled ocean-atmosphere modeling including4-D variational assimilation,simulations in the geosciences, computational manufacturing,and jet acoustics.In order to effectively visualize time-dependent data,it is necessary to store the data at a temporal granularityfine enough to accurately reconstruct the data at any desired time level.Un-fortunately,this is not possible with the simulations we envision.For example,on a24Gigabyte computer,the largest possible simulation of a compressibleflow would have2563grid points assum-ing20arrays of storage with a restartfile of about5Gigabytes.Therefore,a1Terabyte disk can only hold200restartfiles,which is clearly insufficient for temporal post-processing at interactive rates.We are currently developing reduced models of the time-dependent equations that permit a full temporal solution to be reconstructed from the equivalent of30-50time snapshots.Efficient data access techniques based on these models will allow users to interact with their data and visu-alize time-dependent phenomena without recomputing theflow(Gallivan and Van Dooren2000). Instead of saving the full dataset prior to data reduction,the model is computed during the simu-lation.Based on these models,visualization tools are under development to allow users to interact with the data as it is produced by the computation.Concurrent visualization/simulation involves flow visualization in two distinct time intervals.First,the data produced up to the current time is reduced.This is essentially an interpolation andflow-feature extraction task.The second time interval extends from the last simulated time frame to any future time of interest to the user. The emphasis is on the extrapolation offlow features from the available data while retaining a respectablefidelity to the underlying physics.In both time intervals,the number of degrees of freedom must be minimized along with the time it takes to extract characteristic features of the flow.As afirst step,the reduced basis functions will be based on a Karhunen-Loeve decomposi-tion computed incrementally.A discontinuous Galerkin method,built from the original governing equations,is used to compute the reduced set of unknown coefficients.Research in parallel feature extraction is necessary to identify the salient features of the data which will help guide the visualization process and suggest alternate means of efficiently accessing relevant data.On large-scale datasets,parallelism provides a substantial boost to interactive vi-sualization.Examples of features include critical point and vortex cores which have proven to be invaluable in thefluid dynamics community.The most promisingflow visualization techniques to emerge from the research community during the past6years are to automatically placeflow lines(such as streamlines or particle paths)in a dataset(Turk and Banks1996,Jobard and Lefer1997),animate a texture on them(Cabral1993, Kiu and Banks1996,Stalling et al.1997)and illuminate them using a physically-based model derived for1-dimensionalfibers(Banks1994,Zoeckler et al.1997).Thus far,each of these elements has been demonstrated in isolation on research projects.We will integrate them into a complete tool,which promises to provide superior display of time-varying3Dflows.Our recent installation of an8-foot by16-foot display(the“powerwall”)creates an opportunityto investigate advanced techniques in human-computer interaction for visualization of time-varying simulations.We will develop3D interaction tools(“widgets”)to permit scientists to query both qualitative and quantitative information from the scene in an immersive keyboard-free3D envi-ronment.Previous work demonstrated that immersive visualization,with tools for querying data, provided benefit to aflow physicist comparing experimental and numerical data for a turbulent flow(Banks et al.1994,Banks and Singer,1994,Crockett et al.1996).The concurrent visualiza-tion system will provide users with the tools needed to manipulate their data as easily in the time domain as they currently do in the spatial domain(Jobard et al.2000).Given the ability to store a full temporal data set on a local disk with only moderate sacrifice of accuracy,a new set of visual tools will be developed geared towards temporal analysis.2.3Problem Solving Environments2.3.1Application-sensitive compilation and prototypingInvestigators:R.Van Engelen,K.Gallivan,D.Whalley.Two recent projects addressed the need for practical software development environments that consider numerical algorithm spec-ification,implementation,and restructuring at the algebraic/algorithmic level.These projects resulted in two operational environments:Ctadel(Van Engelen,Wolters,and Cats,1997)de-veloped at Leiden University and the Royal Netherlands Meteorological Institute,and falcon (De Rose et al.1996)developed by DeRose,Gallivan,Gallopoulos,Marsolf,and Padua at the University of Illinois at Urbana-Champaign.These software systems are complementary:Ctadel involves the generation of efficient serial,vector,and parallel Fortran codes for non-linear hyperbolic partial-differential equations governing atmospheric models,while falcon is a tool aimed at code generation and optimization of matlab specifications of numerical solvers involved in numerical library prototyping and development.The projects adopt a similar approach:the employment of a high-level problem specification language and an algebraic environment to transform the problem into code by using application-specific information and target hardware specifications.Application-sensitive compilation attempts to unify high-level application-specific algorithm specifications with lower-level compiler technol-ogy to obtain a practical algorithm prototyping and software development environment.This application-sensitive approach addresses the difficulties associated with the inevitable loss of cru-cial semantic information that arises after implementing a particular application solution in a high-level programming language.Loss of semantic information appears to occur on the choice of data structures(structured,unstructured,semi-structured,and sparse matrix representations) and the choice of solvers(direct,iterative,etc.)(van Engelen1997).These choices can have a profound impact on the effectiveness of the parallelization of the application.The Ctadel and falcon projects demonstrated that lifting the abstraction level of the problem specification en-ables the underlying transformation system to algebraically restructure the algorithms and data structures thereby improving run-time performance and scalability of the codes.We will exploit the Ctadel and falcon technology and develop a problem-solving environment (PSE)that includes application-sensitive compilation techniques to facilitate the prototyping of algorithms based on the core algorithm technology for the application projects.In this respect,the PSE differs from the mainstream technologies(ELLPACK for example).Recently we integrated Ctadel with the vpo compiler in an nsf funded project for the au-tomatic validation of code improving transformations(van Engelen,Whalley,Yuan,1999).vpo provides a base for performing data-flow analysis,traditional low-level code-improving transforma-。
[NASA美国太空总署资料(长期更新)].Turbulence.Model.Predictions.of-NASA-aiaa-99-0157
37th Aerospace Sciences Meeting & Exhibit January 11-14, 1999/Reno, NV
For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics 1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344
AIAA-99-0157
TURBULENCE MODEL PREDICTIONS OF EXTRA-STRAIN RATE EFFECTS IN STRONGLY-CURVED FLOWS
Christopher L. Rumsey and Thomas B. Gatskiy NASA Langley Research Center Hampton, Virginia Joseph H. Morrisonz Analytical Services & Materials, Inc. Hampton, Virginia
The abilities of three types of turbulence models to accurately predict the e ects of curvature on ow in a U-duct are studied. An explicit algebraic stress model performs better than one- or two-equation linear eddy viscosity models, although it is necessary to fully account for the variation of the production-todissipation-rate ratio in the algebraic stress model formulation. None of the turbulence models fully captures the suppressed turbulence near the convex wall or enhanced turbulence near the concave wall. However, a full Reynolds stress model predicts the suppressed turbulence near the convex wall. Some of the underlying assumptions used in the development of algebraic stress models are investigated and compared with the computed ow eld from a full Reynolds stress model. Through this analysis, the assumption of Reynolds stress anisotropy equilibrium used in the algebraic stress model formulation is found to be suspect in regions of strong curvature. Many ow elds being calculated by computational uid dynamics CFD codes are so complex that it can be di cult to determine the source of error in comparison with experiment. For example, the ow over a multi-element airfoil contains a wide variety of challenging physical processes, including
Actran_Engine_Intake_Exhaust_acoustics
Engine Intake & Exhaust Acoustic SimulationActran Features and Sample ApplicationsZe Zhou, General Manager AcousticsApril 12, 2016Contents•Introduction to Actran–Company overview–Actran features•Intake& Exhaust Noise Modeling Using Actran –Pipe noise–Shell noise–Flow-induced noise•Sample Applications–Mitsubishi exhaust line–Mazda intake manifold–Sogefi airfilter–Airbus HVAC duct•One slide case studies•Founded in 1998, joined MSC Software in 2011•Headquartered in Brussels, Belgium•Activities:–Development of the Actran software–Services support, training, consulting & technology transfer –Research in acoustic CAE and related fields•More than 300 industrial customers worldwideFree Field Technologies•Noise needs to be studied to:•Accommodate for stringent standards–The standards defined by States are more and more restrictive–It sometimes becomes the dimensioning factor•Improve comfort–Acoustic comfort (car or aircraft cabin for instance)is a marketing argument today:Airbus A380•Prevent damages–In the design of spatial structures,a high level of noise can lead to damages or break-down of the structure•Increasing need for simulation•Prototypes are costly and involved too late in the development cycle•Simulation at the early design phase lead to reduce the development costWhy acoustics ?Evolution of allowed pass-by noise levels from 1970 to 2000646668707274767880828419701977198419922000A c c e p t a b l e l e v e l s (dB )AutomotiveAerospaceMachineryConsumer Goods OtherA few slides to get introduced to ActranThe Actran Software SuiteActran AcousticsActran Vibro-Acoustics Actran Aero-Acoustics Actran TMActran for Trimmed body DMPActran SNGRActranVIActran DGM•Near field: Finite Elements•Far field: Infinite Elements or APML •Radiation of vibrating structures–Engine, gearbox, Manifold, oil pan, turbocharger –Vibrations computed with Nastran, Adams or others•Ducted acoustics–Air inlet, outlet–Silencers, exhaust, ducts with perforated sheet•Interior acoustics:–Interior acoustic of compressor –Noise inside vehicle cabin•Visco-thermal effect, convected propagation •Results provided–Sound pressure, intensity, radiated power–Contribution of different zones to the radiated power –Narrow band, 3rd Octave, dB, dBA.Actran for Acoustic PropagationHeavy duty engine acoustic radiationModel for sound radiation of heavy duty engineFinite/Infinite Elements Around the source: F.EIn far field: I.EEngine with the definition of contribution areasContribution of different areas to the radiated noiseMuffler modelingin Actran•Structure elements–Visco-elastic solid, shell, beam, stiffener –Poro-elastic elements–Rigid body, spring, point mass –Piezo-electric elements•Import of Nastran structural models into Actran •Application examples–Vibro-acoustic analysis of multi-layer structure–Acoustic transparency of windows with frame and seals –Muffler with porous material, shell noise, entire exhaust line –Car cabin noise with trim –Loudspeaker modeling–Vibro-acoustics of a compressor•Results provided–Structural displacement, acceleration, force, stress–Energy dissipated in each layer or each material or any specific area defined by the user Actran for Vibro-Acoustic Simulation (1)Dissipated Energy in each layerof a multi-layer materialVibrations computed by Actranon an aircraft cockpitTransmission loss of awindshield•Two types of shells in Actran–More efficient than solid elements for flexion behavior –Thin shells (2D), thin single-layer structure–Solid shells (3D), for thick multi-layered structures•Coupling with fluid–Strong coupling: fluid and structure interact together –Weak coupling: no retroaction of fluid on structure–Different fluids can be defined in the same model–Support of non-congruent meshes •Modeling of composite materials•Pre-stressed effectMultilayer panel Ship hull vibration Model of Truck muffler•Model foam, rock wool, fibers•Porous elements: based on Biot model–Extensive Poro-Elastic model:with frequency dependent properties•Skeleton properties→Young modulus, density, Poisson ratio•Fluid properties→fluid density•Skeleton/Fluid interaction→tortuosity, resistivity, porosity–Simplified models:Rigid porous, Lump porous, Delaney-Bazley, Miki •Impedance condition, model for perforated sheet•Results provided–Insertion Loss due to the addition of acoustic treatments–Dissipated power in treatments to analyze dissipationmechanisms:•In the skeleton and the fluid of the foamTrim components of aVolkswagen Passat Extensive porous modelingcapabilitiesPorous material on a cardashboard•Study the noise generated by turbulent flows•Based on acoustic analogies–Noise sources are taking into account whatever they are: monopole, dipole, quadruple…–Lighthill for low speed flows–Möhring for mid to high speed flows•Inputs are unsteady or steady CFD-results •Compatible with most CFD softwares (Fluent, CFX, StarCCM+, OpenFoam & others)•Typical applications–HVAC noise, Fan noise•Aero-vibro-acoustic simulations–Cabin noise due to turbulences induced by side mirrors or pillars–When noise due to turbulences excites a structureActran for Aero-Acoustic SimulationUnsteady flow in an HVAC ductNoise produced by HVAC systemPressure fluctuation on windshield and windowsNoise triggered by mown lower bladesExternal steady flows can be used in the acoustic waves propagationTurbulences caused by aside mirror•Standard–Point loads, displacements –Monopoles, plane waves, etc –Distributed loads–Electric excitations (piezo-electric)•Acoustics in far field–Non reflecting boundary condition: similar to an anechoic room –Propagation in far field–Methods: (A)PML, infinite elements•Random excitations–Diffuse sound field: similar to a reverberant room –Turbulent Boundary Layer: Corcos & Goody models –Delta correlated excitation:similar to the rain on the roof•Import–Vibration levels from FEA –Nastran superelement –Unsteady flow from CFDBoundary Conditions & ExcitationsCapability to model an anechoic chamberCapability to model reverberant chamberNoise due to turbulences can be computed from anunsteady CFD•Computational sequences:–Computation in frequency domain•Direct frequency response •Modal frequency response•Hybrid modal-physical response–Computation in time domain -Transient solver –Modal extraction–Time domain LEE Solver (DGM method)–Potential compressible flow solver•Direct & iterative solvers, multiple load & restart •Linux or Windows platforms •HPCActran SolverModal extraction / response forcavity and structureCompressible flow on an aircraft engine air intake: with Actran!Actran is adapted for running on•Pre-processing–Material properties –Boundary conditions –Frequency range –Microphone locations•Post processing–Pressure and displacement maps –Pressure at microphone–Displacement at accelerometers –Mean square pressure and velocity–Generate a sound file of the simulated noise•Interfaced with various mesh formats:Nastran, Ansys , Ideas…•Import of Nastran model •Process automation & scriptingActran Graphical User InterfaceModel set upRadiated noiseAutomatic microphones locations according ISO 3744•Acoustic indicators are directly output with Actran and read in Actran VI–Pressure level in 3rd Octave, dBA, polar directivity–Radiated power with the contribution of different parts of the vibrating component:→to identify the zone to treat, to know the acoustic power of a component –Dissipated power:→to identify the zone, or the layer of a multilayer panel, that dissipates the most acoustic energy –Insertion Loss, Transmission Loss→to evaluate the insulation efficiency of panels / covers –Waterfall diagram:→In automotive, to identify the noise associated to Actran Graphical User InterfaceAcoustic directivityCompatibility with manymeshing toolVibration mode of the window andinterior sound pressure•Goal:–Reduce the dependency to a meshing tool –Automate the acoustic radiation computationfrom a structural mesh create easily / automatically the acoustic model for performing the noise radiation•Typical meshing features available:–Tetrahedral mesh, mesh-on-mesh –Shrink-wrap, convex hull, hole filling –Extrusion–Transformation –Nodes merging•Adaptive meshing–Speed-up the computation•Accurate shrinkwrap–To improve results accuracy–To identify what is the exact par that radiate the mostActran Graphical User Interface: Meshing ToolMeshing tool in ActranShrinkwrap of a powertrainAutomated mesh and set-upfor acoustic radiationIntake& Exhaust Noise Modeling usingActran•Intake and exhaust lines are advantageously modeled with Actran:–3D solver for transfer matrices in cases when analytical expressions are not available–Tailpipe noise•Direct radiation calculation•Evaluation of the radiation impedance at the outlet–Shell noise–Flow-induced noiseIntake and Exhaust Line ModelingInOut (pipe)Out (shell)•Pipe noise–Pure acoustics–Propagation of acoustic waves inside the ducts–Reflections, refraction, diffraction…–Source impedance and amplitude •Shell noise–Coupled vibro-acoustics–The interior acoustics is coupled to the shell vibration•Flow induced noiseWhat can Actran Model?Actran Takes into Account•Excitation–Engine pulsation–Vibration at mount points–Flow turbulence•Physical model–Fluid/structure coupling–Open outlet end–Resonators–Surface coating–Volume absorbent–Perforated pipes–Flow effects–Temperature gradient–Aeroacoustic sourcesPipe Noise Modeling using ActranActran key features for pipe noise•3D solver–Not limited to low frequencies or small ducts–Not limited to simple shapes•Acoustic propagation in mean flow–Import a temperature and a flow field in Actran for convected acoustic propagation •Acoustic duct modes–Provide acoustic excitation–Represents well the semi-infinite anechoic duct–Can be fed with 1D RANS solvers (like GT-Power, WAVE, etc)•Infinite Elements for the free field radiation (pipe end)•Transfer Matrix Method–To split entire line into sub problems and study sub componentsDuct Modes (semi-infinite assumption)•Interior Acoustic Duct = Infinite length = Perfect non reflective condition •In Actran, infinite ducts are modeled analytically (Modal Basis)–Inlet:•Injection of the Plane Mode with a constrained intensity•Free reflection–Outlet:•Free transmissionDuct Modes: A Basic Duct•Characterization of a component of the line (example: muffler) Incident powerfrom the engine Transmitted power (pipe noise)Not reflective BC = analytical duct modes•The Transmission Loss (TL) is calculated–TL: ratio between the incident power (from the engine) and transmitted power (pipe noise) going through a componentTL =10.log10(W incident/W transmitted)•Using the Transfer Matrix Method, the transmission through the entire line can be deduced a posterioriTransmission LossTransmission LossHeterogeneous Media: Temperature effects•The effect of temperature / flow on the local sound speed and density is computed by Actran•The temperature field must be computed at each node location. This can be done by an external CFD code or using Actran with some simplification assumptions600°K300°KEffects of the Temperature –Transmission Loss Transmission LossWith temperatureStrong effect of the temperature•Analytical TMM methods are limited–Simple shapes –Only plane modes–No shell noise , no structure dissipation –Homogenous medium•For more complex modeling, TMM can be used within Actran–Complex geometries–Up to the cut-on frequency of ducts instead of large components –Shell noise + structure dissipation possible –Flow or temperature gradients possibleTransfer Matrix Method (TMM) with ActranTMM analytic codes are limited to the lowest cut-on frequency of all the elements (inlet/outlet/internalduct).Ex :TMM analytic codes can perform the TL computationonly up to 2000Hz.F inlet = 8000HzF internal = 2000HzF outlet 6000HzMix-method (Actran+TMM) can computethe TL until the lowest cut on frequency ofthe inlet/outlet duct.Ex:F inlet = 8000HzF internal = 2000HzIn this case, Actran can perform the TLTask 3: Results recombination using TMMTask 2b: Actran computations–Automation is possible through scripting –The coupling with 1D tools is straightforwardTMM: ProcessTask 2a: Actran Model creationTask 1: Geometry –Division into subsystemsPerformed for each componentValidation of Muffler Transmission LossBasic experimental validationsImprove the design of HVAC components •Transfer matrix of a Y connection and validation :Actran model•Actran is first applied to a simple chamber set-up for validation•The indicator used for the comparison isNR = SPL(Inlet)-SPL(Outlet)Experimental Setup of a Simple ChamberCleaner BOXMicrophone on inletMicrophone on outletSpeaker BOXAcoustic Analysis of Simple ChamberMeas CAE1CAE2Frequency (Hz)RED = CAE1: Point Source N R = I n (d B )-O u t (d B )•A model of air cleaner box is then considered and again validated against experimentsAcoustic Analysis of Air Cleaner BoxNoise SourceMic PointFrequency (Hz)S P L (d B )Experiment Analysis5001000150020dBShell Noise Modeling using ActranActran key features for the shell noise•Structural solver in Actran–Contains basically all features of a classical FEM solver–Shells, solids, etc but also porous materials, multilayered materials–Excellent handling of the damping•Full coupling with the acoustic solver–The structure vibration and the interior acoustics are fully coupled problems –OR hybrid modal-physics solver–OR staggered solver•Many useful features–Incompatible meshes–Fast FRF solver (Krylov) compatible with damping–Connection to MSC Nastran’s super-elements–Energy balance results (ex: energy loss in each component)•FE Model–Fully coupled–Incompatible meshes–Multilayered skin–Interior foam + perforated plates •Excitation:–pulsations at the inlet (e.g. from GT-Power)–Vibration at mounting points–Or both !!A basic exampleFE + IFE meshExterior acousticsShellInterior acousticsStructure deformation Interior cavity SPLEnergies spectraResult TypesExterior sound fieldFlow-Induced Noise Modeling UsingActranHybrid Method•Two decoupled steps–Step 1: compute the unsteady flow using CFD–Step 2: extract sources from the result andpropagate•Assumptions in principle–Main assumption: no interaction between the vortical and acoustic modes–In clear words: the acoustic field does not modify the flow•Challenges–Find the “good” wave operator–Find the “good” source terms–Extract these source terms accurately from CFD inputCAA domain W (Actran, FEM)NRBC at G eW aG e•An unsteady CFD computation (URANS, LES, DNS, …) is used to determine the flow•The sound sources are calculated from these results–Use of Lighthill’s analogy–Standard simplifying assumptionsLighthill’s Analogy: SketchSource domain W s (quadrupoles/dipoles)G sSolid boundary at G sInputs from Unsteady CFD: Actran AeroacousticsInputs from Steady CFD: Actran SNGR MethodValue of SNGR: make use of RANS CFD results, therefore reduce drastically the CFD time required for the subsequent Actran aeroacoustic analsyis•Daimler, Audi, VW, BMW, Porsche have defined a test case: duct + elbow + flap•Measurements (@Dornier) in anechoic room •CFD input: Star-CD results, LES-type •Acoustic computations with ActranApplication Review -German AeroAcoustics Consortium –Test-Case89101167121314151617Phi = 0°Phi = 180°Theta = 0°Theta = 180°。
LMS Virtual.Lab 11流体噪声(气动噪声)文档
Level of turbulence in the flow, characterized by Reynolds number:
ρVL Re μ
Mach
Flow Velocity Sound Speed
Low Re Large flow scales
High Re Large flow scales + smaller flow scales
83m/s (300km/h)
0.24
1 000 000
30m/s
0.09
150 000
The aeolian harp...
Flow-Induced noise simulation - Overview
1 2
3 4
What is Aeroacoustics?
Aeroacoustic Analogy
Ground Transportation
• Pantographs • Train Bogie • Turbulent Boundary Layer window loading • Wiper
Aerospace and Defense
• Landing Gears, Flaps, slats • propellers • Mufflers • Aircraft environmental systems (ECS) • Fuselage Turbulent Boundary Layer loading
“External” Aeroacoustics:
Turbulent flow interacts with rigid body and radiates noise in free space Pantograph, Train bogie, Side mirror
ACTRAN空调研讨会-管道声学分析
技术路线
为了分析和降低噪声,马自达选用了Nastran与ACTRAN联合仿真,预测与
优化进气歧管的噪声水平。
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进气歧管噪声优化分析需要的模块配置
ACTRANforNASTRAN
ACTRANDGM
ACTRANVibro-Acoustics
Copyright Free Field Technologies
Case 2 – 媒质流动的影响– 传递损失
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温度效应
传递损失
温度效应
600K
300K
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排气尾管噪声分析
声固耦合 开放的出口端 消声器 绝热层 吸声材料 穿孔板 流动效应 温度效应
Out (shell) In
Out (pipe)
2
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管道声学分析
管道声传播 管道振动辐射噪声 管道气流再生噪声
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气管道较短,排气系统噪声控制难度较大,必须借助数值分析技术预测 消声器性能并进行优化设计。
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Copyright Free Field Technologies
技术路线
为了分析和降低摩托车排气噪声,铃木使用ACTRAN与其它CFD软件进行联
合仿真,实现快速分析排气噪声问题。
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jstd035声学扫描
JOINT INDUSTRY STANDARDAcoustic Microscopy for Non-HermeticEncapsulatedElectronicComponents IPC/JEDEC J-STD-035APRIL1999Supersedes IPC-SM-786 Supersedes IPC-TM-650,2.6.22Notice EIA/JEDEC and IPC Standards and Publications are designed to serve thepublic interest through eliminating misunderstandings between manufacturersand purchasers,facilitating interchangeability and improvement of products,and assisting the purchaser in selecting and obtaining with minimum delaythe proper product for his particular need.Existence of such Standards andPublications shall not in any respect preclude any member or nonmember ofEIA/JEDEC or IPC from manufacturing or selling products not conformingto such Standards and Publications,nor shall the existence of such Standardsand Publications preclude their voluntary use by those other than EIA/JEDECand IPC members,whether the standard is to be used either domestically orinternationally.Recommended Standards and Publications are adopted by EIA/JEDEC andIPC without regard to whether their adoption may involve patents on articles,materials,or processes.By such action,EIA/JEDEC and IPC do not assumeany liability to any patent owner,nor do they assume any obligation whateverto parties adopting the Recommended Standard or ers are alsowholly responsible for protecting themselves against all claims of liabilities forpatent infringement.The material in this joint standard was developed by the EIA/JEDEC JC-14.1Committee on Reliability Test Methods for Packaged Devices and the IPCPlastic Chip Carrier Cracking Task Group(B-10a)The J-STD-035supersedes IPC-TM-650,Test Method2.6.22.For Technical Information Contact:Electronic Industries Alliance/ JEDEC(Joint Electron Device Engineering Council)2500Wilson Boulevard Arlington,V A22201Phone(703)907-7560Fax(703)907-7501IPC2215Sanders Road Northbrook,IL60062-6135 Phone(847)509-9700Fax(847)509-9798Please use the Standard Improvement Form shown at the end of thisdocument.©Copyright1999.The Electronic Industries Alliance,Arlington,Virginia,and IPC,Northbrook,Illinois.All rights reserved under both international and Pan-American copyright conventions.Any copying,scanning or other reproduction of these materials without the prior written consent of the copyright holder is strictly prohibited and constitutes infringement under the Copyright Law of the United States.IPC/JEDEC J-STD-035Acoustic Microscopyfor Non-Hermetic EncapsulatedElectronicComponentsA joint standard developed by the EIA/JEDEC JC-14.1Committee on Reliability Test Methods for Packaged Devices and the B-10a Plastic Chip Carrier Cracking Task Group of IPCUsers of this standard are encouraged to participate in the development of future revisions.Contact:EIA/JEDEC Engineering Department 2500Wilson Boulevard Arlington,V A22201 Phone(703)907-7500 Fax(703)907-7501IPC2215Sanders Road Northbrook,IL60062-6135 Phone(847)509-9700Fax(847)509-9798ASSOCIATION CONNECTINGELECTRONICS INDUSTRIESAcknowledgmentMembers of the Joint IPC-EIA/JEDEC Moisture Classification Task Group have worked to develop this document.We would like to thank them for their dedication to this effort.Any Standard involving a complex technology draws material from a vast number of sources.While the principal members of the Joint Moisture Classification Working Group are shown below,it is not possible to include all of those who assisted in the evolution of this Standard.To each of them,the mem-bers of the EIA/JEDEC and IPC extend their gratitude.IPC Packaged Electronic Components Committee ChairmanMartin FreedmanAMP,Inc.IPC Plastic Chip Carrier Cracking Task Group,B-10a ChairmanSteven MartellSonoscan,Inc.EIA/JEDEC JC14.1CommitteeChairmanJack McCullenIntel Corp.EIA/JEDEC JC14ChairmanNick LycoudesMotorolaJoint Working Group MembersCharlie Baker,TIChristopher Brigham,Hi/FnRalph Carbone,Hewlett Packard Co. Don Denton,TIMatt Dotty,AmkorMichele J.DiFranza,The Mitre Corp. Leo Feinstein,Allegro Microsystems Inc.Barry Fernelius,Hewlett Packard Co. Chris Fortunko,National Institute of StandardsRobert J.Gregory,CAE Electronics, Inc.Curtis Grosskopf,IBM Corp.Bill Guthrie,IBM Corp.Phil Johnson,Philips Semiconductors Nick Lycoudes,MotorolaSteven R.Martell,Sonoscan Inc. Jack McCullen,Intel Corp.Tom Moore,TIDavid Nicol,Lucent Technologies Inc.Pramod Patel,Advanced Micro Devices Inc.Ramon R.Reglos,XilinxCorazon Reglos,AdaptecGerald Servais,Delphi Delco Electronics SystemsRichard Shook,Lucent Technologies Inc.E.Lon Smith,Lucent Technologies Inc.Randy Walberg,NationalSemiconductor Corp.Charlie Wu,AdaptecEdward Masami Aoki,HewlettPackard LaboratoriesFonda B.Wu,Raytheon Systems Co.Richard W.Boerdner,EJE ResearchVictor J.Brzozowski,NorthropGrumman ES&SDMacushla Chen,Wus Printed CircuitCo.Ltd.Jeffrey C.Colish,Northrop GrummanCorp.Samuel J.Croce,Litton AeroProducts DivisionDerek D-Andrade,Surface MountTechnology CentreRao B.Dayaneni,Hewlett PackardLaboratoriesRodney Dehne,OEM WorldwideJames F.Maguire,Boeing Defense&Space GroupKim Finch,Boeing Defense&SpaceGroupAlelie Funcell,Xilinx Inc.Constantino J.Gonzalez,ACMEMunir Haq,Advanced Micro DevicesInc.Larry A.Hargreaves,DC.ScientificInc.John T.Hoback,Amoco ChemicalCo.Terence Kern,Axiom Electronics Inc.Connie M.Korth,K-Byte/HibbingManufacturingGabriele Marcantonio,NORTELCharles Martin,Hewlett PackardLaboratoriesRichard W.Max,Alcatel NetworkSystems Inc.Patrick McCluskey,University ofMarylandJames H.Moffitt,Moffitt ConsultingServicesRobert Mulligan,Motorola Inc.James E.Mumby,CibaJohn Northrup,Lockheed MartinCorp.Dominique K.Numakura,LitchfieldPrecision ComponentsNitin B.Parekh,Unisys Corp.Bella Poborets,Lucent TechnologiesInc.D.Elaine Pope,Intel Corp.Ray Prasad,Ray Prasad ConsultancyGroupAlbert Puah,Adaptec Inc.William Sepp,Technic Inc.Ralph W.Taylor,Lockheed MartinCorp.Ed R.Tidwell,DSC CommunicationsCorp.Nick Virmani,Naval Research LabKen Warren,Corlund ElectronicsCorp.Yulia B.Zaks,Lucent TechnologiesInc.IPC/JEDEC J-STD-035April1999 iiTable of Contents1SCOPE (1)2DEFINITIONS (1)2.1A-mode (1)2.2B-mode (1)2.3Back-Side Substrate View Area (1)2.4C-mode (1)2.5Through Transmission Mode (2)2.6Die Attach View Area (2)2.7Die Surface View Area (2)2.8Focal Length(FL) (2)2.9Focus Plane (2)2.10Leadframe(L/F)View Area (2)2.11Reflective Acoustic Microscope (2)2.12Through Transmission Acoustic Microscope (2)2.13Time-of-Flight(TOF) (3)2.14Top-Side Die Attach Substrate View Area (3)3APPARATUS (3)3.1Reflective Acoustic Microscope System (3)3.2Through Transmission AcousticMicroscope System (4)4PROCEDURE (4)4.1Equipment Setup (4)4.2Perform Acoustic Scans..........................................4Appendix A Acoustic Microscopy Defect CheckSheet (6)Appendix B Potential Image Pitfalls (9)Appendix C Some Limitations of AcousticMicroscopy (10)Appendix D Reference Procedure for PresentingApplicable Scanned Data (11)FiguresFigure1Example of A-mode Display (1)Figure2Example of B-mode Display (1)Figure3Example of C-mode Display (2)Figure4Example of Through Transmission Display (2)Figure5Diagram of a Reflective Acoustic MicroscopeSystem (3)Figure6Diagram of a Through Transmission AcousticMicroscope System (3)April1999IPC/JEDEC J-STD-035iiiIPC/JEDEC J-STD-035April1999This Page Intentionally Left BlankivApril1999IPC/JEDEC J-STD-035 Acoustic Microscopy for Non-Hermetic EncapsulatedElectronic Components1SCOPEThis test method defines the procedures for performing acoustic microscopy on non-hermetic encapsulated electronic com-ponents.This method provides users with an acoustic microscopy processflow for detecting defects non-destructively in plastic packages while achieving reproducibility.2DEFINITIONS2.1A-mode Acoustic data collected at the smallest X-Y-Z region defined by the limitations of the given acoustic micro-scope.An A-mode display contains amplitude and phase/polarity information as a function of time offlight at a single point in the X-Y plane.See Figure1-Example of A-mode Display.IPC-035-1 Figure1Example of A-mode Display2.2B-mode Acoustic data collected along an X-Z or Y-Z plane versus depth using a reflective acoustic microscope.A B-mode scan contains amplitude and phase/polarity information as a function of time offlight at each point along the scan line.A B-mode scan furnishes a two-dimensional(cross-sectional)description along a scan line(X or Y).See Figure2-Example of B-mode Display.IPC-035-2 Figure2Example of B-mode Display(bottom half of picture on left)2.3Back-Side Substrate View Area(Refer to Appendix A,Type IV)The interface between the encapsulant and the back of the substrate within the outer edges of the substrate surface.2.4C-mode Acoustic data collected in an X-Y plane at depth(Z)using a reflective acoustic microscope.A C-mode scan contains amplitude and phase/polarity information at each point in the scan plane.A C-mode scan furnishes a two-dimensional(area)image of echoes arising from reflections at a particular depth(Z).See Figure3-Example of C-mode Display.1IPC/JEDEC J-STD-035April1999IPC-035-3 Figure3Example of C-mode Display2.5Through Transmission Mode Acoustic data collected in an X-Y plane throughout the depth(Z)using a through trans-mission acoustic microscope.A Through Transmission mode scan contains only amplitude information at each point in the scan plane.A Through Transmission scan furnishes a two-dimensional(area)image of transmitted ultrasound through the complete thickness/depth(Z)of the sample/component.See Figure4-Example of Through Transmission Display.IPC-035-4 Figure4Example of Through Transmission Display2.6Die Attach View Area(Refer to Appendix A,Type II)The interface between the die and the die attach adhesive and/or the die attach adhesive and the die attach substrate.2.7Die Surface View Area(Refer to Appendix A,Type I)The interface between the encapsulant and the active side of the die.2.8Focal Length(FL)The distance in water at which a transducer’s spot size is at a minimum.2.9Focus Plane The X-Y plane at a depth(Z),which the amplitude of the acoustic signal is maximized.2.10Leadframe(L/F)View Area(Refer to Appendix A,Type V)The imaged area which extends from the outer L/F edges of the package to the L/F‘‘tips’’(wedge bond/stitch bond region of the innermost portion of the L/F.)2.11Reflective Acoustic Microscope An acoustic microscope that uses one transducer as both the pulser and receiver. (This is also known as a pulse/echo system.)See Figure5-Diagram of a Reflective Acoustic Microscope System.2.12Through Transmission Acoustic Microscope An acoustic microscope that transmits ultrasound completely through the sample from a sending transducer to a receiver on the opposite side.See Figure6-Diagram of a Through Transmis-sion Acoustic Microscope System.2April1999IPC/JEDEC J-STD-0353IPC/JEDEC J-STD-035April1999 3.1.6A broad band acoustic transducer with a center frequency in the range of10to200MHz for subsurface imaging.3.2Through Transmission Acoustic Microscope System(see Figure6)comprised of:3.2.1Items3.1.1to3.1.6above3.2.2Ultrasonic pulser(can be a pulser/receiver as in3.1.1)3.2.3Separate receiving transducer or ultrasonic detection system3.3Reference packages or standards,including packages with delamination and packages without delamination,for use during equipment setup.3.4Sample holder for pre-positioning samples.The holder should keep the samples from moving during the scan and maintain planarity.4PROCEDUREThis procedure is generic to all acoustic microscopes.For operational details related to this procedure that apply to a spe-cific model of acoustic microscope,consult the manufacturer’s operational manual.4.1Equipment Setup4.1.1Select the transducer with the highest useable ultrasonic frequency,subject to the limitations imposed by the media thickness and acoustic characteristics,package configuration,and transducer availability,to analyze the interfaces of inter-est.The transducer selected should have a low enough frequency to provide a clear signal from the interface of interest.The transducer should have a high enough frequency to delineate the interface of interest.Note:Through transmission mode may require a lower frequency and/or longer focal length than reflective mode.Through transmission is effective for the initial inspection of components to determine if defects are present.4.1.2Verify setup with the reference packages or standards(see3.3above)and settings that are appropriate for the trans-ducer chosen in4.1.1to ensure that the critical parameters at the interface of interest correlate to the reference standard uti-lized.4.1.3Place units in the sample holder in the coupling medium such that the upper surface of each unit is parallel with the scanning plane of the acoustic transducer.Sweep air bubbles away from the unit surface and from the bottom of the trans-ducer head.4.1.4At afixed distance(Z),align the transducer and/or stage for the maximum reflected amplitude from the top surface of the sample.The transducer must be perpendicular to the sample surface.4.1.5Focus by maximizing the amplitude,in the A-mode display,of the reflection from the interface designated for imag-ing.This is done by adjusting the Z-axis distance between the transducer and the sample.4.2Perform Acoustic Scans4.2.1Inspect the acoustic image(s)for any anomalies,verify that the anomaly is a package defect or an artifact of the imaging process,and record the results.(See Appendix A for an example of a check sheet that may be used.)To determine if an anomaly is a package defect or an artifact of the imaging process it is recommended to analyze the A-mode display at the location of the anomaly.4.2.2Consider potential pitfalls in image interpretation listed in,but not limited to,Appendix B and some of the limita-tions of acoustic microscopy listed in,but not limited to,Appendix C.If necessary,make adjustments to the equipment setup to optimize the results and rescan.4April1999IPC/JEDEC J-STD-035 4.2.3Evaluate the acoustic images using the failure criteria specified in other appropriate documents,such as J-STD-020.4.2.4Record the images and thefinal instrument setup parameters for documentation purposes.An example checklist is shown in Appendix D.5IPC/JEDEC J-STD-035April19996April1999IPC/JEDEC J-STD-035Appendix AAcoustic Microscopy Defect Check Sheet(continued)CIRCUIT SIDE SCANImage File Name/PathDelamination(Type I)Die Circuit Surface/Encapsulant Number Affected:Average%Location:Corner Edge Center (Type II)Die/Die Attach Number Affected:Average%Location:Corner Edge Center (Type III)Encapsulant/Substrate Number Affected:Average%Location:Corner Edge Center (Type V)Interconnect tip Number Affected:Average%Interconnect Number Affected:Max.%Length(Type VI)Intra-Laminate Number Affected:Average%Location:Corner Edge Center Comments:CracksAre cracks present:Yes NoIf yes:Do any cracks intersect:bond wire ball bond wedge bond tab bump tab leadDoes crack extend from leadfinger to any other internal feature:Yes NoDoes crack extend more than two-thirds the distance from any internal feature to the external surfaceof the package:Yes NoAdditional verification required:Yes NoComments:Mold Compound VoidsAre voids present:Yes NoIf yes:Approx.size Location(if multiple voids,use comment section)Do any voids intersect:bond wire ball bond wedge bond tab bump tab lead Additional verification required:Yes NoComments:7IPC/JEDEC J-STD-035April1999Appendix AAcoustic Microscopy Defect Check Sheet(continued)NON-CIRCUIT SIDE SCANImage File Name/PathDelamination(Type IV)Encapsulant/Substrate Number Affected:Average%Location:Corner Edge Center (Type II)Substrate/Die Attach Number Affected:Average%Location:Corner Edge Center (Type V)Interconnect Number Affected:Max.%LengthLocation:Corner Edge Center (Type VI)Intra-Laminate Number Affected:Average%Location:Corner Edge Center (Type VII)Heat Spreader Number Affected:Average%Location:Corner Edge Center Additional verification required:Yes NoComments:CracksAre cracks present:Yes NoIf yes:Does crack extend more than two-thirds the distance from any internal feature to the external surfaceof the package:Yes NoAdditional verification required:Yes NoComments:Mold Compound VoidsAre voids present:Yes NoIf yes:Approx.size Location(if multiple voids,use comment section)Additional verification required:Yes NoComments:8Appendix BPotential Image PitfallsOBSERV ATIONS CAUSES/COMMENTSUnexplained loss of front surface signal Gain setting too lowSymbolization on package surfaceEjector pin knockoutsPin1and other mold marksDust,air bubbles,fingerprints,residueScratches,scribe marks,pencil marksCambered package edgeUnexplained loss of subsurface signal Gain setting too lowTransducer frequency too highAcoustically absorbent(rubbery)fillerLarge mold compound voidsPorosity/high concentration of small voidsAngled cracks in package‘‘Dark line boundary’’(phase cancellation)Burned molding compound(ESD/EOS damage)False or spotty indication of delamination Low acoustic impedance coating(polyimide,gel)Focus errorIncorrect delamination gate setupMultilayer interference effectsFalse indication of adhesion Gain set too high(saturation)Incorrect delamination gate setupFocus errorOverlap of front surface and subsurface echoes(transducerfrequency too low)Fluidfilling delamination areasApparent voiding around die edge Reflection from wire loopsIncorrect setting of void gateGraded intensity Die tilt or lead frame deformation Sample tiltApril1999IPC/JEDEC J-STD-0359Appendix CSome Limitations of Acoustic MicroscopyAcoustic microscopy is an analytical technique that provides a non-destructive method for examining plastic encapsulated components for the existence of delaminations,cracks,and voids.This technique has limitations that include the following: LIMITATION REASONAcoustic microscopy has difficulty infinding small defects if the package is too thick.The ultrasonic signal becomes more attenuated as a function of two factors:the depth into the package and the transducer fre-quency.The greater the depth,the greater the attenuation.Simi-larly,the higher the transducer frequency,the greater the attenu-ation as a function of depth.There are limitations on the Z-axis(axial)resolu-tion.This is a function of the transducer frequency.The higher the transducer frequency,the better the resolution.However,the higher frequency signal becomes attenuated more quickly as a function of depth.There are limitations on the X-Y(lateral)resolu-tion.The X-Y(lateral)resolution is a function of a number of differ-ent variables including:•Transducer characteristics,including frequency,element diam-eter,and focal length•Absorption and scattering of acoustic waves as a function of the sample material•Electromechanical properties of the X-Y stageIrregularly shaped packages are difficult to analyze.The technique requires some kind offlat reference surface.Typically,the upper surface of the package or the die surfacecan be used as references.In some packages,cambered packageedges can cause difficulty in analyzing defects near the edgesand below their surfaces.Edge Effect The edges cause difficulty in analyzing defects near the edge ofany internal features.IPC/JEDEC J-STD-035April1999 10April1999IPC/JEDEC J-STD-035Appendix DReference Procedure for Presenting Applicable Scanned DataMost of the settings described may be captured as a default for the particular supplier/product with specific changes recorded on a sample or lot basis.Setup Configuration(Digital Setup File Name and Contents)Calibration Procedure and Calibration/Reference Standards usedTransducerManufacturerModelCenter frequencySerial numberElement diameterFocal length in waterScan SetupScan area(X-Y dimensions)Scan step sizeHorizontalVerticalDisplayed resolutionHorizontalVerticalScan speedPulser/Receiver SettingsGainBandwidthPulseEnergyRepetition rateReceiver attenuationDampingFilterEcho amplitudePulse Analyzer SettingsFront surface gate delay relative to trigger pulseSubsurface gate(if used)High passfilterDetection threshold for positive oscillation,negative oscillationA/D settingsSampling rateOffset settingPer Sample SettingsSample orientation(top or bottom(flipped)view and location of pin1or some other distinguishing characteristic) Focus(point,depth,interface)Reference planeNon-default parametersSample identification information to uniquely distinguish it from others in the same group11IPC/JEDEC J-STD-035April1999Appendix DReference Procedure for Presenting Applicable Scanned Data(continued) Reference Procedure for Presenting Scanned DataImagefile types and namesGray scale and color image legend definitionsSignificance of colorsIndications or definition of delaminationImage dimensionsDepth scale of TOFDeviation from true aspect ratioImage type:A-mode,B-mode,C-mode,TOF,Through TransmissionA-mode waveforms should be provided for points of interest,such as delaminated areas.In addition,an A-mode image should be provided for a bonded area as a control.12Standard Improvement FormIPC/JEDEC J-STD-035The purpose of this form is to provide the Technical Committee of IPC with input from the industry regarding usage of the subject standard.Individuals or companies are invited to submit comments to IPC.All comments will be collected and dispersed to the appropriate committee(s).If you can provide input,please complete this form and return to:IPC2215Sanders RoadNorthbrook,IL 60062-6135Fax 847509.97981.I recommend changes to the following:Requirement,paragraph number Test Method number,paragraph numberThe referenced paragraph number has proven to be:Unclear Too RigidInErrorOther2.Recommendations forcorrection:3.Other suggestions for document improvement:Submitted by:Name Telephone Company E-mailAddress City/State/ZipDate ASSOCIATION CONNECTING ELECTRONICS INDUSTRIESASSOCIATION CONNECTINGELECTRONICS INDUSTRIESISBN#1-580982-28-X2215 Sanders Road, Northbrook, IL 60062-6135Tel. 847.509.9700 Fax 847.509.9798。
Modeling the Acoustic Channel for Simulation Studies
DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.Modeling the Acoustic Channel for Simulation StudiesDr. Michele Zorzi, PIDepartment of Information EngineeringUniversity of PadovaVia Gradenigo, 6/B – 35131 Padova, Italyphone: +39-049-827-7762 fax: +39-049-827-7699 email: zorzi@dei.unipd.itAward Number: N000141010422http://telecom.dei.unipd.it/pages/read/75/LONG-TERM GOALSUnderwater acoustic communications, especially from a single point-to-point link perspective, have been studied extensively in the past few decades. Underwater networking issues have begun to attract the interest of researchers as well, and represent a fertile research area which can be expected to grow in the future. Bringing the study of acoustic communications systems to the networking level has the potential to open up new directions and to provide a means to make them much more powerful and useful. Many military and naval applications can be expected to greatly benefit from this paradigm shift.The main goal of the proposed work is to develop channel modeling techniques to enable more detailed studies at the networking level. To this aim, we propose to start from existing data sets for point-to-point communications, in order to try and extract fundamental behaviors and model them in a way suitable for the simulation of more complex systems. This includes the integration of existing (as well as new) acoustic propagation modeling techniques into network simulators, the search for synthetic statistical models based on measured data, as well as the development of trace-based simulation techniques, and their validation and assessment.OBJECTIVESAs the project started on 04/01/10, the reporting period covers the first five months of the effort. The main objective for the first six months was to gain a detailed understanding of the propagation phenomena that most affect underwater acoustic systems, and to identify the main sources of available experimental data that can be used for our purposes. This preliminary investigation is instrumental for the core research activities of the project, to be carried out during the rest of the first and through the second year, in which data analysis techniques will be used in order to identify key behaviors and to provide synthetic models for the acoustic channel, to be thoroughly validated against measured data. APPROACHThe objective of the proposed research work is to develop simulation models able to correctly capture the behavior of acoustic propagation in underwater communication networks, while containing theproper level of detail that makes them realistic while still sufficiently lightweight for use in networking simulations.The technical approach we proposed to adopt in the overall effort includes the following points: (i) deep interdisciplinary understanding of acoustic propagation environments and networking capabilities/requirements; (ii) identification and evaluation of the main PHY metrics that need to be used in networking studies; (iii) development of comprehensive simulation models that accurately reproduce the propagation characteristics of underwater channels, while also being suitable for use in networking studies; (iv) validation of the proposed models in the performance analysis of advanced communications and networking functionalities through detailed analysis, simulation, and experimentation.In this first part of the project (five months), we mostly focused on point (i) above, and on starting some interactions with other research groups who can give us access to experimental datasets.The current project team includes Prof. Michele Zorzi (PI), Prof. Gianfranco Pierobon (co-PI), Dr. Paolo Casari (post-doctoral researcher) and Ms. Beatrice Tomasi (Ph.D. student).WORK COMPLETEDThe focus of the work in these first five months of the project has been the following: (i) to develop some detailed understanding on acoustic propagation; (ii) to further develop our WOSS simulation framework; (iii) to interact with groups who may be able to give us access to experimental datasets which we can analyze.Point (i) required some literature study as well as observations based on real data and on the output of detailed propagation software tools, e.g., Bellhop [BH]. Although we of course cannot claim we have become experts in ocean acoustics, which is an exceedingly complex topic, we are confident that our understanding of acoustic propagation phenomena is adequate for the tasks we need to accomplish in this project.As to point (ii), we have rounded up a version of the World Oceans Simulation System (WOSS) [WOSS], which provides a handy interface to mediate between the well-known network simulator ns2 and the propagation simulation tool Bellhop. In general any network simulator takes care of managing high-level node behavior (adherence to protocol rules, mobility, on/off periods, position updates, and so forth), while delegating the management of transmission/reception events to a different part of the code or to external modules. In any event, the network simulator itself expects an output from channel signaling as to whether a transmission was successful or not, how much interference it created to (or received from) other nodes, and which node could correctly receive or overhear it. This entails a characterization of the attenuation that signals incur as they travel throughout the network.WOSS is an instrument which provides exactly one such output, by triggering more realistic simulation of acoustic propagation through Bellhop. Since Bellhop needs environmental data, WOSS gathers this data given knowledge of the geographic position of the nodes in the world, as well as of the period of the year where network operations are assumed to take place. Such information is readily obtained from the network simulator. After that, WOSS queries ocean databases for environmental parameters such as a seasonal average of the sound speed profile, the sea bottom and surface waves profile, as well as the type of bottom sediments, and provides this data to Bellhop, which outputs anestimate of the transmission loss incurred by acoustic waves. Optionally, the user can ask WOSS to average the transmission loss over different realizations of the SSP (random surface wave generation is in the process of being implemented). New features have been recently implemented in WOSS. These allow, among other things, to include knowledge of the emission pattern of the transducer in use. The transducer itself can be chosen among a variety of commercial models of common use, covering many possible frequency bands. All of the above has been released in the public domain under an open source licence, and can be downloaded (along with proper documentation)from http://telecom.dei.unipd.it/ns/woss/The interactions with other research groups and the search for datasets to be used in our analysis (point (iii)) have been mostly focused in four directions, namely, SeaWeb, NUS, WHOI and NURC.Some preliminary contacts have been made with Prof. Joe Rice (Naval Postgraduate School) and Dr. Chris Fletcher (SPAWAR), both of the SeaWeb project, and with Prof. Mandar Chitre’s group at the National University of Singapore (NUS). We are still discussing the possibility to access some of the datasets they gathered through multiple sea trials in the recent past. We have met Prof. Joe Rice in Venice last July, and will be having additional interactions. We also plan to meet NUS representative at ACM WUWNET at the end of September.We are now interacting rather closely with Woods Hole Oceanographic Institution (WHOI). We are in contact with Dr. Jim Preisig, who has given us access to datasets obtained in some of his ONR-funded efforts. Beatrice Tomasi has just started a semester at WHOI as a visiting PhD student, and will be working with Jim on channel models, data analysis, and experiment design. Michele Zorzi and Paolo Casari will also be visiting WHOI in September. We believe that this collaboration with WHOI will lead to very good results.Finally, we have a long-time relationship with the NATO Undersea Research Centre (NURC). We have been interacting heavily with them in the past two years, and have done some collaborative work on underwater protocol design and analysis, which is related to the present project. In addition, we participated in a sea trial campaign (SubNet09) in the Summer of 2009, and again in September 2010. Some details about the experimental results and some initial data analysis efforts are described in the next section.RESULTSThe results obtained in the SubNet09 sea trials represent a very comprehensive dataset that we have started to analyze. Even though such results were not produced as part of the current effort, they currently represent the main starting point of our investigation. In the following, we provide some information about the experimental setting and some preliminary observations.The experiments were performed off the coast of the island of Pianosa, Italy (42.585_N, 10.1_E), and spanned a period of about three and a half months, between May and September 2009.The testbed consisted of four hydrophones arranged at different depths in a vertical array (VA), and of three acoustic modems (all Teledyne-Low Frequency models [Tele]) placed on a tripod on the sea floor at a depth of 60, 70 and 80m, at different distances from the VA (1500m, 2200m and 700m, respectively).A scheme of the testbed is depicted in Figure 1 [OCEANS10]. The three transmitters have been labeled T1 (1500m from the VA, depth 60m), T2 (2200m from the VA, depth 70m) and T3 (700m from the VA, depth 80m). The hydrophones of the VA (named H1, H2 and H4 – hydrophone H3 wasnot working properly unfortunately), are placed at 20, 40 and 80m, respectively. Temperature sampling in the water column close to the VA was provided by a thermistor chain and, combined with a CDT measurement, allowed to derive the sound speed profile (see Figure 2).Fig. 1: A scheme of the testbed deployment off the coast of the Pianosa Island.Fig. 2: Average and standard deviation of SSP during experiments on May 30,June 5 and September 2.Results obtained from such experiment include for example the time evolution of the channel impulse response for the different links (see Figure 3), which makes it possible to study coherence times as well as temporal and spatial correlations of the channel behaviors.Fig. 3: Pseudocolor plot of measured channel impulse response amplitudesfor the link between T3 and H4.Other interesting data that will be used in our study include the time series of SNR values (which is useful in studying time-correlations, see Figure 4) and the experimentally derived relationship between SNR and PER (which is important in deriving the communication performance, see Figure 5).Figure 4: Measured time series of the SNR over the links from all transmitters to hydrophoneH1, including a moving average taken over 25 samples.Figure 5: Log-scale scatterplot of PER as a function of SNR for varying transmitterand all receivers. Linear fits are also provided.This large dataset will be analyzed in order to obtain useful statistical information (that will help in characterizing both qualitatively and quantitatively the channel behaviors).IMPACT/APPLICATIONSWe expect the results obtained from the analysis of such a comprehensive dataset to greatly improve our understanding and modeling capabilities, which is a key goal in our project.RELATED PROJECTSDuring the reporting period, the PI has not had any active related project sponsored by ONR or the US government. He has had some related efforts funded by the European Commission, an Italian foundation, and NATO. The focus of such efforts is more on protocol design than on channel modeling and therefore those projects are complementary and non-overlapping with respect to the present one. REFERENCES[BH] M. Porter et al., “Bellhop code.” [Online]. Available: http://oalib./Rays/index.html[WOSS] F. Guerra, P. Casari, and M. Zorzi, “World Ocean Simulation System (WOSS): a simulation tool for underwater networks with realistic propagation modeling,” in Proc. of WUWNet 2009, Berkeley, CA, Nov. 2009.[Tele] “Teledyne benthos undersea systems and equipment,” .[OCEANS10] B. Tomasi, G. Zappa, K. McCoy, P. Casari, and M. Zorzi, “Experimental study of the space-time properties of acoustic channels for underwater communications,” in Proc. IEEE/OES Oceans , Sydney, Australia, May 2010. PUBLICATIONS Given the short time the project has been running, we have no publications that carry an explicit acknowledgement to it. However, the following recent papers contain material that is relevant to the project’s objectives and have been published and/or accepted during the reporting period:• Beatrice Tomasi, Giovanni Zappa, Kim McCoy, Paolo Casari, Michele Zorzi, “Experimental study of the space-time properties of acoustic channels for underwater communications,” in Proc. IEEE/OES Oceans , Sydney, Australia, May 2010.• Beatrice Tomasi, Laura Toni, Paolo Casari, Lorenzo Rossi, Michele Zorzi, “Performance Study of Variable-Rate Modulation for Underwater Communications based on Experimental Data,” • Beatrice Tomasi, Paolo Casari, Leonardo Badia, Michele Zorzi, “ in Proc. MTS/IEEE Oceans , Seattle, USA, Sep. 2010.A Study of Incremental Redundancy Hybrid ARQ over Markov Channel Models Derived from Experimental Data,”•Beatrice Tomasi, Paolo Casari, Lorenzo Finesso, Giovanni Zappa, Kim McCoy, Michele Zorzi, “ in Prof. of ACM WUWNet , Woods Hole, USA, Sep.-Oct. 2010.On Modeling JANUS Packet Errors over a Shallow Water Acoustic Channel using Markov and Hidden Markov Models ,” in Proc. IEEE MILCOM , San Jose, USA, Nov. 2010. HONORS/AWARDS/PRIZES Michele Zorzi:• IEEE Fellow, 2007• Member-at-Large of the IEEE Communications Society Board of Governors, 2009-2011 • Editor-in-Chief of the IEEE Transactions on Communications, 2008-present• Editor-in-Chief of the IEEE Wireless Communications magazine, 2003-2005• Editor for Europe of the Wiley Journal on Wireless Communications and Mobile Computing • Keynote Speaker, European Wireless conference, Lucca, Italy, Apr. 2010. (Address was on protocol design issues and channel modelling in underwater acoustic networks.)• Best Paper Award, IEEE MobiWac Workshop, June 2005• Best Paper Award, IEEE CAMAD, June 2006• Best Paper Award, IEEE GLOBECOM (Wireless Networks Symposium), November 2007 • Best Tutorial Paper Award, IEEE Communications Society, 2007• Best Paper Award, European Wireless Conference, May 2009•Guest Editor of several special issues, and in particular: “Underwater Acoustic Communications and Networks,” IEEE Journal on Selected Areas in Communications, December 2008)•Member of the organizing and technical program committees of many conferences, and in particular: Technical Program co-Chair, ACM WUWNet’07。
03-ACTRAN气动声学模块介绍
其中w(t)是窗函数
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窗函数
原始信号q(t)
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窗函数
Actran中的窗函数
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CA 节点 (稀疏)
信息丢失
积分插值法:
CFD 节点 (致密) 从CFD节点到CA网格的积分插值
CA 节点 (稀疏)
所有信息都被利用,避免信息丢失! ◄
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窗函数
频谱能量泄漏
执行DFT,需要截断有限信号片段考虑部分的信号
ACTRAN DGM
ACTRAN VibroAcoustics
ACTRAN AeroAcoustics
ACTRAN TM
ACTRAN Acoustics ACTRAN VI 4
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ACTRAN Aero-Acoustics
包含所有针对流致噪声仿真分 析的高级属性
限制
源项不够精确 数值成本不可忽略(大量涡模态=大量计算)◄
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简要回顾CFD技术
DNS:直接数值模拟
解决所有尺度 DNS是不实际的
LES: 大涡模拟 解决大尺度结构,包含大多数能量 建模小尺度对大尺度结构的影响
无霜冰箱风道的振动分析及改进
第40卷第1期声学技术Vol.40, No.1引用格式:韩宝坤, 甘信伟, 鲍怀谦, 等. 无霜冰箱风道的振动分析及改进[J]. 声学技术, 2021, 40(1): 97-103. [HAN Baokun, GAN Xinwei, BAO Huaiqian, et al. Vibration analysis and improvement of air duct of frost-free refrigerator[J]. Technical Acoustics, 2021, 40(1): 97-103.] DOI: 10.16300/ki. 1000-3630.2021.01.015无霜冰箱风道的振动分析及改进韩宝坤1,甘信伟1,鲍怀谦1,2,王鹏1,刘泽坤1,贾思祥1(1. 山东科技大学机械电子工程学院,山东青岛266590;2. 青岛澳柯玛股份有限公司,山东青岛266510)摘要:文章以无霜冰箱风道为研究对象,通过有限元模拟对风道固有频率、谐波响应和LMS b振动试验进行分析,得到了风道壳体的固有频率、振幅极限和试验模态。
计算结果表明,在风机工况状态下,风道振动噪声幅度最大时的频率是在风机工作的基频附近,通过风道粘贴阻尼的方式降低振幅,进而降低风道壳体传递给冰箱箱体的辐射噪声。
试验结果表明:在风道壳体振幅最大的区域粘贴阻尼材料后,在半消声室进行噪声测试,冰箱整体减振效果明显且噪声级降低了1.9 dB。
文章为风道减振降噪的改进提供方向和建议。
关键词:风道;振动噪声;模态分析;谐波响应;LMS振动试验中图分类号:TB535 文献标志码:A 文章编号:1000-3630(2021)-01-0097-07Vibration analysis and improvement of air duct offrost-free refrigeratorHAN Baokun1, GAN Xinwei1, BAO Huaiqian1,2, W ANG Peng1, LIU Zekun1, JIA Sixiang1(1. College of Mechanical and Electronic Engineering, Shandong University of Science and Technology, Qingdao 266590, Shandong, China;2. Qingdao Aokoma Co., Ltd., Qingdao 266510, Shandong, China)Abstract: In this paper, the air duct of the frost-free refrigerator is taken as the research object. The natural frequency analysis, harmonic response analysis and LMS b vibration test of the air duct are conducted by finite element simulation, and the natural frequency, amplitude limit and experimental mode of the air duct shell are obtained. The calculation results show that the frequency of the strongest vibration of air duct is close to the fundamental frequency of the fan, and the vibration amplitude can be reduced by pasting damping materials on the air duct, thereby the radia-tion noise transmitted from the duct shell to the refrigerator box is reduced. The experimental results show that after the damping materials are pasted on the area of the air duct shell with the largest vibration amplitude, the vibration of the whole refrigerator is obviously weakened and the radiated noise level is reduced by 1.9 dB according to the test in a semi-anechoic chamber. This paper provides a direction and suggestions for reducing vibration and noise in air duct.Key words: air duct; vibration noise; modal analysis; harmonic response; LMS vibration test0 引言随着社会的快速发展,居民消费水平的提升,对大容量、多功能高端冰箱的需求越来越多,目前冰箱风冷制冷方式虽然达到了对制冷量的需求,但是风扇旋转产生强烈的振动,噪声影响较为严重。
一种声学换能器改进实频数据宽带匹配算法
第9卷第3期2020年5月网络新媒体技术Vol.9No.3May 2020一种声学换能器改进实频数据宽带匹配算法*周跃涛1,2,3黄海宁1,2(1中国科学院声学研究所北京1001902中国科学院先进水下信息技术重点实验室北京1001903中国科学院大学北京100190)摘要:提出一种对声学换能器进行宽带匹配设计的改进实频数据优化算法。
该算法避免了繁琐的数学运算,并有效降低了优化过程的非线性度,提高了优化的效率。
在对该算法进行理论分析的基础上,举例说明了经过匹配之后,声学换能器的工作带宽明显拓宽,功率增益也明显提高。
关键词:声学换能器,宽带匹配,优化算法,实频数据Improved Real Frequency Algorithm based for BroadbandMatching of Acoustic Emission TransducerZHOU Yuetao 1,2,HUANG Haining 1(1Institute of Acoustic ,Chinese Academy of Sciences ,Beijing ,100190,China ,2Key Laboratory of Science and Technology on Advanced Underwater Acoustic Signal Processing ,Chinese Academy of Sciences ,Beijing ,100190,China ,3University of Chinese Academy of Sciences ,Beijing ,100190,China )Abstract :An improved Real Frequency data optimization algorithm for broadband matching design of acoustic transducers is presented in this paper ,which avoids tedious mathematical operations ,and effectively reduces the non -linearity of the optimization process and improves the optimization efficiency.On the basis of theoretical analysis of the algorithm ,an example is given to illustrate that after matching ,the working bandwidth of the acoustic transducer is obviously broadened and the power gain is improved.Keywords :Acoustic transducer ,Broadband matching ,Optimization algorithm ,Real frequency data本文于2019-01-04收到。
中国管道标准
DL/T 4412004
火力发电厂高温高压蒸汽
管道蠕变监督规程
()
DL/T 50311994(2005)
电力建设施工及验收技术
规范(管道篇)
()
DL/T 50541996(2005)
火力发电厂汽水管道设计
技术规定
()
DL/T 51212000
火力发电厂烟风煤粉管道
设计技术规程
()
DL/T 52042005
Buried Polyethylene(PE) piping systems for the supply of gaseous fuels Part 2:Fittings
GB 17428- 通风管道的耐火试验方法 Fire resistance test method
1998
of ventilation ducts
的定义和选用
Pipework componentsDefinition and selection of PN
GB/T 11790-1996
设备及管道保冷技术通则
General principles for lowtemperature insulation technique of equipments and pipes
()
管道焊接接头超声波检验
技术规程
()
钢制承压管道对接焊接接
头射线检验技术规范
()
火力发电厂蒸汽管道寿命
/links/pipe/gb.htm
2009-8-11
中国管道标准(GB pipe standards)
页码,2/20
2005
DL/T 9822005
Pipework componentsDefinition and selection of DN (norminal size)
TM_1_Coupling_Duct_Modes-ACTRAN管道模态理论
p p
p
p-
At low frequencies, only the plane wave propagates inside the duct At higher frequencies, the acoustic field can be more complex In any case, the pressure can be seen as a mathematical superposition of duct modes (this is an exact representation)
If kz is real real, one can say that the mode (m (m,n) n) is cut cut-on on (or propagating) If kz is imaginary , the mode amplitude will vanish following z direction. The mode is cut-off or evanescent
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Context
To g get accurate boundary y conditions and excitations mechanisms is of major importance for numerical models. For aero-acoustic problems occurring in ducts, ACTRAN provides two main i ways to d define fi the h excitation i i :
flueng acoustics modeling_fluent 声学分析教程
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Fluent User Services Center
Advanced Acoustics Modeling FLUENT v6.2 Jun 2005
Aeroacoustic Source Classification
Fluent User Services Center
Advanced Acoustics Modeling FLUENT v6.2 Jun 2005
Aeroacoustics – What do we expect?
Source Information Strength, contribution from different sources, source classification Propagation Accurate tracking of acoustic waves Receiver Receiver signal (acoustic pressure) Spectra, shape of spectra (broadband, tones) Receiver Acoustic Medium Flow Sound, Acoustic Radiation
A relationship between density and pressure. This relationship, affected by temperature, determines the speed of sound within the medium: The motion of the medium itself, e.g., wind. Independent of the motion of sound through the medium, if the medium is moving, the sound is further transported. The viscosity of the medium. This determines the rate at which sound is attenuated. For many media, such as air or water, attenuation due to viscosity is negligible.
博士生申请学位发表学术论文的规定
博士生申请学位发表学术论文的规定为促进我校博士研究生科研能力与学术水平的提高,保证博士学位论文的质量,博士研究生申请学位论文送审前发表的学术论文须符合以下规定:一、博士研究生以第一作者发表的学术论文须与学位论文相关,且符合各学院的要求(附后);满足学院要求的学术论文中,须至少有1篇学术论文已公开发表,理工科类博士研究生其中须至少有1篇学术论文用英文发表。
二、在《华南理工大学学报》和其他高校学报,以及华南理工大学主办的其他学术期刊上发表的多篇论文只统计1篇,在学术会议上发表多篇会议论文只统计1篇,且各学科认可的学术会议上发表的学术论文须被SCI/EI收录。
(法学院、思想政治学院另行规定内容见附表)三、博士研究生以本人为第一作者在本学科国际重要学术期刊上发表1篇学术论文,视为达到申请学位发表学术论文的要求。
四、博士研究生以第一发明人获得授权的与学位论文研究内容相关的发明专利相当于1篇SCI/EI收录的学术论文(计算机科学与工程学院、轻工科学与工程学院、食品科学与工程学院、机械与汽车工程学院另行规定,环境与能源学院博士生不适用于本款内容)。
五、如无特殊说明,认可的期刊目录以录用时的版本为准,且不含增刊、特刊、专刊等;JCR分区及SCI影响因子以录用、发表或提交审核时的最新版本为准;JCR分区指大类分区。
六、提交审核的学术论文网络在线发表(即具有DOI号、在网络可查阅文章全文)视为公开发表。
七、被录用的学术论文应有编辑部的正式录用函和导师签名的论文投稿原件。
八、论文第一作者/专利第一发明人是指博士研究生本人署名第一,或者导师署名第一、本人署名第二;论文第一署名作者指博士研究生本人署名第一;论文的第一署名单位/专利申请人单位必须是华南理工大学。
九、博士研究生申请答辩时,如果其提交审核的学术论文中尚有正式录用但未公开发表(或发明专利申请公开但未正式授权)的,允许其组织学位论文答辩,答辩通过者,经所在学院学位评定分委员会审议可先准予毕业,但暂不审议其学位,待其在毕业后两年内所提交审核的学术论文全部公开发表(或专利授权)后,再由本人提出申请审议其学位。
国内外有关振动噪声研究的主要机构
国内外有关振动噪声研究的主要机构yifeng911 发表于: 2007-10-13 21:36 来源: 中国振动联盟刚刚入门,向各位前辈请教一下,国内外有关振动噪声研究的主要机构有哪些呀???最新回复VibrationMaster at 2007-10-14 07:17:08Acoustical Laboratories: (with links WWW)ArgentinaLaboratório de Acustica e ElectroacústicaAustralia:CSIRO group at Sidney, Acoustics and Surface MechanicsCausal Systems Pty Ltd - Adelaide, SA, AustraliaBenelux:Ghent Acoustics pageIPO, Center for Research on User-System Interaktion Eindhoven University of TechnologyLaboratory of Seismics & Acoustics at DelftCanada:Acoustics & Vibration at Sherbrooke UniversityChina:Shanghai Jiao Tong UniversityDenmark:Department of Acoustics Technology Technical University of Denmark, Copenhagen Department of Communication Technology Aalborg University, DenmarkFinland:Acoustics Lab Helsinki University of TechnologyFrance:Laboratoire de mechanique et d'acoustique de Marseille, part of France's Centre Naional deRecherche Scientifique (en français)IRCAMLaboratoire Ondes et AcoustiqueCentre d'Information et de Documentation sur le BruitCentre Acoustique - Ecole Centrale de LyonLaboratoire Vibrations AcoustiqueGermany:Department of Acoustics of the Carl von Ossietzky-University OldenburgInstitute of Technical Acoustics of the RWTH-AachenInstitute of Technical Acoustics of the TU-DresdenAuditory Research Group in DarmstadtConference ServerIreland:Sound and Vibrations group Trinity College, DublinItaly:NATO SACLANTCEN La SpeziaNew Zealand:Psychophysics Lab at Victoria University of WellingtonARC ATS (Auckland)Norway:NAS The Acoustical Society of NorwayNORSIG The Norwegian Society for Signal ProcessingNOTAM Norwegian network for Technology, Acoustics and MusicAcoustics Group TrondheimSINTEF DELAB TrondheimDepartment of Physics University of BergenSignal Processing Group Høgskolen i StavangerTelenor ForskningPoland:Cybernetic Acoustics at Polish Academy of SciencesInstitute of Telecommuncation and Acoustics Wroclaw Technical UniversityPortugal:Acoustical Laboratory at the Faculty of Engineering of the University of PortoSpain:Instituto de Acústica's WWW Acoustics Server Research Laboratory in MadridSweden:The Marcus Wallenberg Laboratory for Sound and Vibration Research The Royal Institute ofTechnology, StockholmDepartment of Applied Acoustics Chalmers University of Technology, Göteborg, also availableis the Department's Annual ReportDepartment of Speech, Music and Hearing The Royal Institute of Technology, Stockholm Institutionen for signalbehandling Högskolan i Karlskrona/RönnebyUnited Kingdom:Access to all of theInstitute of Physics Publishing magazines and newslettersISVR Institute of Sound and Vibration Research, SouthamptonUnderwater Acoustics/Medical ultrasonics at BathUltrasonic and Acoustic Transducer Group at SouthamptonHomepage from Douglas Nunn at Durham University (good links to other sites)U.S.A.:Acoustics & Vibration at MIT (good links to other sites)Cochlear Physiology Group at MITAuditory List at MIT, contains JASA and JASP issues and ASA Meetings abstractsHearing Sciences or Auditory Perception Lab at BerkeleyCochlear MechanicsInner Ear anatomySpeech Language Programs in Pathology/Audiology in the U.S.Duke University Adaptive Structures Lab - duct/structural/aero acousticsParmly Hearing Institute Loyola UniversityPenn State - Acoustics WWW page or the Centre for Acoustics and VibrationAcoustics at Auburn University AlabamaThe Vibro-Acoustics Consortium University of KentuckyCochlear Fluids Research Lab Washington UniversityBerkeley Active Noise Control LabOcean Acoustics Lab MassachusettsSandia National Laboratories Research FacilitiesResearch Laboratory Penn StateNASAAcoustics at NASATOPS Group at Nasagopher for STI database - acoustics/ultrasonicsReturn to Top--------------------------------------------------------------------------------National Acoustical Societies in the world:Argentina Acoustical Association / Asociacion de Acusticos Argentinosc/o Prof A. Mendez, Laboratorio de Acustica, Camino Centenario Y 506,1897 - Gonnet, ArgentinaTel: +54 21 84 2686 Fax: +54 21 71 2721Australian Acoustical Society sitePrivate Bag 1, Darlinghurst, NSW 2010AustraliaTel: +61 2 331 6920 Fax: +61 2 331 7296Austrian Acoustics AssociationC/o Prof. Ewald Benes, Technical University of Wien, Institut fur Allgemeine Physik, WienAustriaTel: +43 1 58801-5587 Fax: +43 1 5864203Belgian Acoustics Association (ABAV)Av. P Holoffe 21, 1342 LimeletteBelgiumTel: +32 2 653 88 01 Fax: +32 2 653 07 29Brazilian Acoustics Society / Sociedade Brasileira de AcústicaAttn Prof Samir Gerges, Universidade Federal de Santa Catarina, Departamento de Engenharia Mecânica, Campus Universitário, C.P 476CEP 88040-900, Florianópolis - SCBrazilTel: +55 48 23444074 Fax: +55 48 2341524SOBRAC Web siteCanadian Acoustical AssociationPO Box 1351, Station F, Toronto, Ontario, M4Y 2V9, CanadaTel: +1 514 343 7559 or +1 613 993 0102Web siteAcoustical Society of China17 Zhongguancun St., Beijing 100080ChinaCroatian Acoustical SocietyA/c Dr. Branko SomeckFaculty of Electrical Engineering, Dep. of ElectroAcoustics, Unska 3 HR-41000 ZagrebCroatiaTel: +385.1.62.629640 Fax: +385.1.629862Czech Acoustical Societyc/o Ondrej Jiricek, Technicka 2, 166 27 Prague 6Czech RepublicTel: +42 2 24352310 Fax: +42 2 3111786WebsiteAcoustical Society of Denmarkc/o The Acoustics Laboratory, Bldg. 352 - Technical Universityof Denmark, DK-2800 LyngbyDenmarkTel: +45 4588 1622 Fax: +45 4588 0577Acoustical Society of Finlandc/o Helsinki University of Technology, Acoustics Laboratory,Otakaari 5 A, SF-02150 EspooFinlandTel: +358 04511 xt 2490WebsiteFrench Acoustical Society / Société Française d'Acoustique23 avenue Brunetière, 75017 ParisFranceTel +33 1 48 88 90 59 Fax: +33 1 48 88 90 60Web siteGerman Acoustical Society / Deutsche Gesellschaft für Akustikc/o Department of Physics Acoustics, University of Oldenburg,D-26111 OldenburgGermanyTel: +49 441 798 3572 Fax: +49 441 798 3698Web siteHellenic Acoustical SocietyPatision 147, 112 51 AthensGreeceTel or Fax: +30 1 8646 065Hungarian Society / OPAKFI-Scientific Society for Optics, Acoustics Motion Pictures andTheatre TechnologyFö u. 68 Budapeste, H-1027HungaryTel or Fax: +361 185 1780Acoustical Society of India (c/o National Physical Lab.)c/o Dr S Agrawal, CEERI Centre, CSIR Complex, Hillside Road,New Delhi-110012IndiaTel: +91 11 5784642Italian Association of Acoustics / Associazione Italiana di Acusticavia Cassia 1216, 00189 RomaItalyTel: +39 6 30365765 Fax: +39 6 30365341Acoustical Society of Japan / Nippon Onkyo Gakkai4th Floor, Ikeda Building, 2-7-7 Yoyogi, Shibuya-ku, TokyoJapanTel: +81 3 3379 1200 Fax: +81 3 3379 1456The Acoustical Society of Koreac/o 302-B, The Korean Federation of Science and Technology, 635-4, Yeoksam-dong, Kangnam-gu, Seoul-city, 135-080, Rep. of KoreaTel: +82 2 565 1625 Fax: +82 2 569 9717Latvian Acoustical Commissionweb siteMexican Institute of Acoustics / Instituto Mexicano de Acusticac/o Sergio Beristain, P.O. 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Carlos Jimenez D., Garcilaso de la Vega, 163Salamanca de Monterrico, Lima 3, PeruPolish Acoustical Society / Polskie Towarzystow AkustykiInstytut Akustyki, Uniwersytet Adama Mikiewicz, ul J.Matejki 48/49,60-769 PoznanPolandSociedade Portuguesa de Acústica / Portuguese Society of Acoustics LNEC-LaboratórioNacional de Engenharia CivilP-1700-066 LisboaPortugalTel. +351.218443273 Fax. +351.218443028Grupo de Estudos em Acústica/ Group of Acoustical StudiesAcoustical Lab., Dep. of Civil Eng., Fac. Eng. University of PortoR. 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Box 912-169, SilvertonSouth Africa, 0127Tel or Fax: +27 12 832857Spanish Acoustical Society / Sociedad Española de AcusticaSerrano 144, 28006 MadridSpainTel: +34 1 5618806 Fax: +34 1 4117651Swedish Acoustical Society / Svenska Akustiska Sallskapetc/o Tor Kihlman, Chalmers Univerity of Technology, Dept. of Applied AcousticsS-412 96, GothenburgSwedenTel: +46 31 7722200 Fax: +46 31 7722212Swiss Acoustical Societyweb siteTurkish Acoustical SocietyTel: +90 212 293 1340 xt 2234 Fax: +90 212 264 4237Institute of Acoustics5 Holywell Hill, St Albans, Herts, AL1 1EU, UKTel: +44 1727 848195 Fax: +44 1727 850553Web siteAcoustical Society of America500 Sunnyside Blvd., Woodbury, NY 11797U.S.A.Tel: +1 516 576 2360 Fax: +1 516 576 2377Web SiteInstitute of Noise Control Engineering (INCE)PO Box 3206 Arlington Branch, Poughkeepsie, NY 12603U.S.A.Tel: +1 914.462.4006 Fax: +1 914.463.0201Web SiteReturn to Top--------------------------------------------------------------------------------Federations of National Acoustical Societies:EAA-European Acoustics AssociationLehrstuhl AEA Ruhr-Universitat Bochum D-44780 BochumTel: +49 234 700 2496 Fax: +49 234 7094 165Web siteFIA-Federação IberoAmericana de Acústica A/c Prof. Samir Gerges, Universidade Federal de Santa Catarina, Departamento de Engenharia Mecânica, Campus Universitário, C.P 476 CEP 88040-900, Florianópolis - SC, BrasilTel: +55 48 23444074 Fax: +55 48 2341524International Commission on AcousticsWeb site。
双层微穿孔管消声器传声损失理论计算与分析
双层微穿孔管消声器传声损失理论计算与分析张孟浩;左曙光;相龙洋;胡佳杰【摘要】基于-维平面波理论和微穿孔结构吸声理论,推导双层微穿孔管消声器传声损失理论模型,并将理论计算值与三维有限元声学仿真结果进行对比,利用消声器传声损失理论公式,对比双层和单层微穿孔管消声器的传声损失,分析内外层膨胀腔厚度对双层微穿孔管消声器声学特性的影响.研究结果表明:双层微穿孔管消声器在中低频的传声损失要大于单层微穿孔管消声器;增加内外层膨胀腔的厚度,可以提高双层微穿孔管消声器的消声特性;当双层膨胀腔总厚度固定,外层膨胀腔厚度大时,消声器在中低频的声学性能更好.【期刊名称】《中南大学学报(自然科学版)》【年(卷),期】2015(046)002【总页数】7页(P505-511)【关键词】平面波理论;双层微穿孔管消声器;传声损失;膨胀腔厚度【作者】张孟浩;左曙光;相龙洋;胡佳杰【作者单位】同济大学新能源汽车工程中心,上海,201804;同济大学新能源汽车工程中心,上海,201804;同济大学新能源汽车工程中心,上海,201804;同济大学新能源汽车工程中心,上海,201804【正文语种】中文【中图分类】TB535.2微穿孔板吸声结构具有高声阻和低声抗的特点,因而具有良好的吸声效果。
其吸声理论的正确性已得到学者们的验证,并被广泛采用[1−5]。
微穿孔板具有清洁、无污染及不受材料限制的优点,近年来被制作成管结构,应用于消声器结构。
由于双层微穿孔板结构的吸声效果要比单层微穿孔板结构的更好,学者们开始利用双层微穿孔管消声器进行消声,并取得良好的降噪效果[6]。
目前,国内外均没有直接计算微穿孔管消声器声学特性的理论公式,只是通过微穿孔板结构的吸声理论来设计消声器[7−8]。
而微穿孔板吸声系数并不能很好地说明微穿孔管消声器的声学特性。
因此,有必要提出微穿孔管消声器声学特性的理论模型,进行消声器的结构设计。
微穿孔管消声器与穿孔管消声器消声原理类似,只是结构的声阻抗不同。
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Advances in the acoustics of flow ducts and muflers
59
The transfer matrices used in the aforesaid articles assumed plane wave propagation in a stationary inviscid medium. The problem of wave propagation in a viscous medium involves a coupling of radial and axial components of acoustic particle velocity in the Navier-Stokes equations as well as the continuity equation. This was solved to obtain the analytical expressions for the acoustic pressure attenuation constant, (complex) wave number, and (complex) characteristic impedance. These results were then applied to analyse waves in branched pipes of the hydraulic brake system excited by periodic pumping (Kant et a1 1974). In the case of engine muflers, waves propagate in a moving medium. In order to account for the convective effect of mean flow, a new set of state variables, convective pressure p, and convective mass velocity vc were defined to replace the classical variables of acoustic pressure p and acoustic mass velocity, v. It turned out that the two sets of variables are related linearly to each other as follows:
58
M L Munjal
and current, and due consideration was given to the radiation impedance Zo (of the atmosphere at the tail-pipe end), and source characteristics p, and Z,, analogous to the load impedance, open circuit voltage and internal impedance of the source, respectively. Evaluation of insertion loss of an 11-element filter for a sinusoidai signal by means of the classical method involves simultaneous solution of 2n t 2 algebraic equations. Therefore, a comprehensive transfer matrix method was developed for one-dimensional linear dynamical systems which would include mechanical systems (vibration isolators), electrical wave filters and acoustical filters. In the process, the natural frequency equation, modal vectors and the criteria for forced response of filters (viz., transmission loss, insertion loss and transmissibility) were expressed in terms of a single nondimensional parameter, called velocity ratio (VR) (Munjal et al 1973b). Figure 1 shows two equivalent representations of the electrical analogous circuit of an acoustical filter, and velocity ratio, VR, is defined as
Siidhand, Vol. 15, Part 2, September 1990, pp. 57-72.
0 Printed in India.
Advances in the acoustics of ow ducts and mufflers
M L MUNJAL
Department of Mechanical Engineering, Indian Institute of Science, Bangalore 560 012, India MS received 14 May 1990 Abstract. This review paper deals with advances made in the last two decades in the acoustics of flow ducts for heating, ventilation and air-conditioning (HVAC) systems and engine mumers. The context, concepts, methods used and .results have been highlighted. Frequency-domain one-dimensional analysis of reflective mumers has been emphasized because of its basic importance and wide application. Finally, problems needing further research have been identified. Keywords. Acoustics; mufflers; noise control; engines; HVAC systems; duct acoustics.
where elements are numbered from load to the source, point n is immediately upstream of the nth element, and it is assumed that all the n elements are passive. In figure 1, p,, and Z , , are the source characteristics p, and Z,, respectively. In the proposed transfer matrix method the filter response is given in terms of the velocity ratio VR,,,, which can be evaluated by successive multiplication of n t 2 (2 x 2) matrices. Making use of a heuristic study (with mathematical induction) of the process of the transfer matrix multiplication, an algebraic algorithm was developed for evaluation of the velocity ratio VR,,, (figure Ib). The algorithm permits the set of most significant terms at a particular frequency of interest to be identified from a knowledge of the relative magnitudes of the impedances of the constituent elements of a proposed configuration (Munjal et al 1973~). This feature was then made use of for arriving at some general criteria for synthesis of one-dimensional acoustic filters (Munjal et a1 1973a) and multi-degree-of-freedom vibration isolators (Munjal 1975b).
,
,
Pn+l
an n-element
ttt
an n-element
Z"+I P,Jn
I
firr
r+
1
(b)
Figure 1. A filter with its terminations. (a) Pressure representation for the source; @) Velocity representation for the source.
Ua
1. Introduction Exhaust noise of automotive engines is the main component of the noise pollution of the urban environment. With the ever-increasing population density of vehicles on the road, this has become an important area of research and development. Most of the advances in the theory of acoustic filters and exhaust mufflers have come about in the last three decades, and the author of this article has been active in this area for over two decades. For a monograph on the acoustics of ducts and mufflers see Munjal (1987a). This article, following the monograph in format, briefly reviews the work done by him independently and jointly with his colleagues and students, and relates it to the state-of-the-art. Finally, further problems awaiting solution are identified for future research in the area. 2. Frequency-domain one-dimensional analysis of reflective mufflers