Discussion of EQUI-energy sampler by Kou, Zhou and Wong
双水相体系在化学反应工程中的应用研究进展
广东化工2021年第5期· 62 · 第48卷总第439期双水相体系在化学反应工程中的应用研究进展林锦良,余贵山,李友凤*(遵义师范学院化学与化工学院,贵州遵义563000)[摘要]双水相体系作为化学反应介质具有操作方便、组分可调、绿色环保、连续操作和易于工艺放大等特点,引起了界面科学、分离提纯和反应工程等研究和应用领域的广泛研究。
基于上述优点,本文将对双水相体系在氢化反应、加氢酰胺化反应、耦联反应、聚合反应、CO2还原反应,无膜电池设计和新型纳米材料制备的应用分别进行综述,结合新材料开发、清洁能源利用和环境可持续性发展等研究进行分析,将为相关的研究领域提供参考和启示。
[关键词]双水相体系;化学反应;清洁能源;纳米材料[中图分类号]TQ [文献标识码]A [文章编号]1007-1865(2021)05-0062-03Advances of Aqueous Two Phase System (ATPS) Applications on ChemicalReaction EngineeringLin Jinliang, Yu Guishan, Li Youfeng*(Department of Chemistry and Chemical Engineering Zunyi Normal College, Zunyi 563000, China) Abstract: Aqueous Two Phase Systems (ATPS) has attracted tremendous attentions in the field of interracial science, separation and purification, and chemical reaction engineering due to their various advantages of facility, adjustable, sustainable, continuous operation and large scale industrial adaptive when they were employed as chemical reaction medium. The chemical reactions including hydrogenation, hydroamidation, oxidation, coupling reaction, polymerization, CO2 reduction etc. taken in the ATPS have been reviewed in the paper. Besides, the membrane-free cell and Ag particles has also been covered. Thereafter, the discussions on exploitation of clean energy and preparation of novel materials base on the ATPS have also been presented. All these efforts should provided a significance on the relevant researches.Keywords: Aqueous Two Phase System(ATPS);Chemical Reaction;Clean Energy;Nano Material双水相体系(ATPS)是将两种不同组分的水溶液以一定浓度混合而形成互不相溶的两相系统。
ISE电解质电род说明书
Epoxy body combination ISE electrodes afford a unique ease of use. They measure free ions in aqueous solution quickly, simply, accurately and economically. The sealed reference design eliminates the need to add filling solutions and minimizes reference dryout. 1. The electrode is shipped in a protective plastic bottle. Chloride(Cl -) is shipped with pH4 buffer solution in the bottle. , Nitrate(NO3-), Fluoride (F -), Potassium(K +) and Ammonium (NH 4+) ISE are shipped dry. The electrode should remain in the bottle until it is ready for use. If the electrode is used infre-quently, the bottle and its solution should be saved and the electrode stored in it (See Electrode Storage Section). Take out electrode by loosening plastic top on bottle counterclockwise and pulling electrode out. Slide cap and o-ring off electrode and save (SEE FIGS 1 & 2).2. Stir the electrode in the sample, standard, or rinse solution. This action will bring solution to the electrode's sur- face quicker and improve the speed of response.3. Use these electrodes for aqueous samples only . Samples with organic solvents can dissolve ISE membranes.4. Keep standards and samples at the same temperature. This action will eliminate the need to correct values for temperature effects.5. Keep in mind that all ISE electrodes can change with use. This is characterized by shortened span (slope) and slower speed of response. Check the measuring surface to see if it is dirty. Follow cleaning instructions in page 3 to remove build up on the electrode's sensing surface. HELPFUL OPERATING TIPSPolymer Body, Sealed Combination ISE Electrodes Product InstructionsREQUIRED EQUIPMENT1. ISE meter or pH meter with mV setting2. ISE electrode3. DI water4. Calibration standardsCALIBRATION PROCEDUREThe frequency of calibration is a function of the electrode, the meter, and the solutions the electrode is exposed to. The elec-trode and meter should always be calibrated together with the calibration frequency determined by experience. Use at least two standard solutions bracketed around the measuring range (example: range = 10-800ppm, standards = 1ppm and 1000ppm)---The value you must differ by a factor of 10x or more . Make sure all standard solutions are at the same temperature.1. Remove the electrode from its soaker bottle and the save the bottle.2. Rinse the electrode in deionized water and blot dry3. Stir the electrode in the lowest concentration standard and record the reading once it stabilizes (mV if manual cal or press cal button for meter with ISE mode).4. Repeat Step 2.5. Stir the electrode in the next higher (or highest if only per-forming a 2-point calibrattion)concentration standard and record the reading once it stabilizes (mV if manual cal or press cal button for meter with ISE mode)..ELECTRODE SPECIFICATIONS Dimensions: 6.50" (165 mm) H x 0..476"(12 mm) OD Wetted Materials:ISE pellet (F-, Cl-)(NH4+, NO3-, K+)I SEmembraneEpoxyBody:Silicone/PellonJunction: Temperature Range: 0-60°C (F-, Cl- only)(NH4+, NO3-, K+)0-40°CIsopotential Point: NH4+ = 0 +/-20mV (1ppm)K+ = 0 +/-20mVF- = 240 +=/-20mVNO3- = 200 +/-20mVCl- = 225 +/-20mV (10ppm)e: 56 +/-4mVSloppH Range: Cl- : 2 -10 pHNH4+: 4 -10 pHNO3 - : 3-11 pHK+:3-11 pHF- : 5-7 pHConcentration Range: Cl- : 5x10-5 to 1MNH4+: 1 x 10-6 to 1MNO3 - : 7 x 10-6 to 1MK+: 1 x 10-6 to 1MF- : 1 x 10-5 to 1MResponse Time: 90% in1 minuteInterferring ions:NH4+ = K+. Li+, Na+, Cs+K+ = Cs+, NH4+, H+, Li+, Na+, Ag+F-OH-, H+ complexes=Cl-, NO2-, Br-, CN-, ClO3-, I-, ClO4-=NO3-S-2, I-, Br-, CN-, OH-=CL-。
insight - energy analysis
insight - energy analysisEnergy analysis is the process of examining energy usage and identifying ways to increase efficiency and reduce waste. It involves collecting and analyzing data related to energy consumption, costs, and performance, and using that information to make informed decisions and implement strategies for energy conservation and management.One key insight from energy analysis is identifying patterns and trends in energy usage. By analyzing energy data over specific time periods, such as hourly, daily, or monthly, it is possible to identify peak demand times, patterns of usage, and areas of high energy consumption. This information can help in optimizing energy usage, avoiding peak demand charges, and identifying opportunities for energy-saving measures.Another insight that can be gained from energy analysis is understanding the impact of different factors on energy usage. By evaluating the relationship between energy usage and variables such as weather conditions, production output, occupancy rates, or operating hours, it becomes possible to identify how these factors affect energy consumption. This insight can be used to implement energy-saving measures and make more accurate energy-related decisions.Furthermore, energy analysis can provide insights into the effectiveness of energy-saving measures and technologies. By comparing energy consumption before and after implementing specific measures or technologies, it is possible to evaluate their impact, identify successful strategies, and prioritize investments.This insight can help in developing long-term energy management plans and determining which measures provide the most significant energy and cost savings.Overall, energy analysis provides valuable insights into energy usage, efficiency, and opportunities for optimization. By understanding patterns and trends, evaluating the impact of different factors, and assessing the effectiveness of measures, organizations and individuals can make more informed decisions regarding energy conservation and management, leading to reduced energy costs and environmental benefits.。
argumentation sample1
A sample from students:Welcome to Disney Land in ShanghaiWith the accelerating development of economic and the deepening of Reform and Open-up, China has become the third largest entity. Embracing multi-cultures and integration into globalization are the inexorable trend.To begin with, Disney Land to be built in Shanghai will boost the employment in face of tough job market globally. Substantial investments worth of billions of dollars, beyond question, will be like the fuel in snowy weather. Its economic connotation speaks for itself.Obviously, another benefit will be spiritual enjoyment and cultural amusement. Without going abroad, Chinese people can admire and appreciate exotic cultures, let alone numerous cartoon figures such as Mickey Mouse and Donald Duck. Moreover, the traveling expenditure of saving from abroad journeys will afford many admission tickets.(教师按:此句与整段不一致,应归为经济方面)Moreover, this will be another golden opportunity to elevate Shanghai’s international metropolis image, aside from the 2010 World Expo.As the bellwether of China, Shanghai has been vying with Tokyo, Hong Kong and Singapore to become the economic and financial hub of the Asian-Pacific region. Introduction of Disney Land will not only advance the adjustment of industrial structure, but further raise Shanghai’s competitive power culturally.Undeniably, with this matter will emerge a few issues. But weighing the pros and cons, I believe Disney Land to be built in Shanghai will be a correct choice, not only for Shanghai, but also for China.教师注:红色为主题句,蓝色为支撑句,黄色为有问题部分,下划线为闪光点。
Computation of the Flow of Thermally Perfect Gas Past a Supersonic Projectile with Base Ble
Computation of the Flow of Thermally Perfect Gas Past aSupersonic Projectile with Base BleedPetri KaurinkoskiHelsinki University of Technology,Laboratory of AerodynamicsSähkömiehentie4,FIN–02150,Espoo,FINLAND This paper deals with Navier–Stokes simulations for a supersonic projectile with base bleed.A separate species continuity equation is solved for the bled gas in order to obtain detailed information about the mixing of the jet and the externalflowfield.A thermodynamic model based on curve-fit equations for the specific heats of the individual species is developed to describe accurately the properties of the mixture.Since the mixture is not a-priori homogeneous,the construction of the model is done locally for each computational cell during every iteration cycle.Results for three geometries are presented at two Mach numbers with two base-bleed specifications.1IntroductionTrajectory simulations for artillery projectiles can nowa-days be carried out quickly on any personal computer.The reliability of the simulation depends on the accuracyof the atmospheric model and the accuracy of the aero-dynamic model of the projectile.As a matter of fact,one important task in the simulation of theflight of anartillery projectile is to determine its aerodynamic prop-erties.The aerodynamics may be determined by exper-imental or theoretical putational Fluid Dy-namics(CFD),representing the latterfield,is becomingan important tool in determining theflight properties ofprojectiles.During the past few years,techniques employing dif-ferent types of jets for controlling theflight of aircrafts1and projectiles2,3have been developed.With projec-tiles,the practical aim is to extend thefiring range,i.e.to reduce the base drag by bleeding gas from thebase of the shell.In order to accelerate the design pro-cess of a projectile with base bleed,numerical simula-tions can be used for comparing different design options.There are,however,many unanswered questions regard-ing the reliability of the numerical simulations:Turbu-lence modelling always incorporates some uncertainty,and the thermodynamic as well as chemical properties ofthe bled gas are probable sources of errors.In this paper we present results of Navier–Stokessimulations for a supersonic projectile with base bleed.splitting of Roe is applied for the inviscidfluxes and the thin-layer approximation is used for the friction terms. The effects of turbulence are taken into account using Chien’s low-Reynolds-number model.The FIN-FLO code is described in more detail in Kaurinkoski et. al.6In comparison with results from previous simula-tions employing the Baldwin–Lomax turbulence model as well as experimental results for comparable projec-tiles,the present simulations overpredict the drag of the shells.2Numerical Method2.1Governing Equations in DifferentialFormThe Reynolds-averaged Navier–Stokes equations,and the equations for the kinetic energy and dissipation of turbulence,and the scalar transport equation can be written in the following form(1) where.The in-viscidfluxes are(2)Here,is the density,is the velocity, is the pressure,and is a scalar variable describing,e.g.,the concentration of a species or the mass fraction of a species.The total internal energy is defined as(6) where is a turbulent viscosity coefficient.In the mo-mentum and energy equations,the kinetic energy contri-bution has been connected with pressure and appears in the convectivefluxes.The viscous terms contain a lami-nar and a turbulent part.Similarly,the heatflux is written as(7) where is the temperature,and is the energyflux due to diffusion of mass.7The pressure is calculated from anequation of state,which,for a calorically perfect gas,is written(13) In order to avoid unphysical growth of the turbulent vis-cosity,e.g.,near the stagnation point,we limit the production of turbulent kinetic energy as suggested by Menter9(14)According to the tests conducted,9the maximum of the ratio inside shear-layers is about two,and therefore this limit should not affect the well–behaving regions of theflowfield.Only the problems encountered near the stagnation point should disappear.In addition,this lim-iter has some effect on the solution of shock waves. The equations for and contain empirical coeffi-cients.These are given by(15) where the turbulence Reynolds number is defined as(17) for an arbitraryfixed region with a boundary.Per-forming the integrations for a computational cell yieldscell surface.In this way,only the Cartesian form of theflux is needed.This is calculated from(21)where and are the solution vectors evaluated on the left and right sides of the cell surface,the righteigenvector of the Jacobian matrix,the corresponding eigenvalue is,and is the corresponding characteristic variable obtainedfrom,where.A MUSCL-type approach has been adopted for the evaluation ofand.In the evaluation of and,primitiveflow variables,and conservative turbu-lent variables are utilized.2.4Calculation of the Viscous Fluxes andthe Source TermThe viscousfluxes are evaluated using a thin-layer ap-proximation,which is applied in the curvilinear coordi-nate system.In the computer code,the thin-layer model can be activated in any coordinate direction.For the derivatives in the production term of turbulent kinetic en-ergy(12),however,the thin-layer model is not applied. Instead,the derivatives are calculated exactly.The possible wall corrections of the turbulent viscos-ity,as well as those of the source terms,are calculated separately in the,and directions.As a result,the source term may contain several wall correction terms, and the wall damping of turbulent viscosity is a product of the different wall-damping terms in different coordi-nate directions if several walls are present.2.5Boundary ConditionsAt the free-stream boundary,the values of the depen-dent variables are kept as constants.However,in regions where the free-stream velocity is directed out from the computational domain,the boundary values are extrapo-lated.In theflowfield,and are limited from below to their free-stream values.In the calculation of the inviscid fluxes at the solid boundary,theflux-difference splitting is not used.Since the convective speed is equal to zero on the solid surfaces,the only contribution to the invis-cid surfacefluxes arises from the pressure terms in the momentum equations.A second-order extrapolation is applied for the evaluation of the wall pressure as(22) where the subscript refers to conditions on the wall, and and refer to the centre of thefirst and second cell from the surface,respectively.A similar formula is used for the diffusion coefficients on the wall.The viscousfluxes on the solid surfaces are obtained by setting on the wall.The central expression of the viscous terms is replaced by a second-order one-sided formula.(23) where is the thickness of thefirst cell on the surface. The boundary condition for the energy equation can be determined in two ways:either the wall temperature is set to a pre-defined temperature,or the wall is assumed to be adiabatic.In this work,the latter method is employed. The viscousfluxes of and,as well as,are also set to zero at the wall.In this way there is no need to specify the surface values of the turbulence quantities.2.6Specification of the Inlet BoundaryConditionsThe base-bleed boundary is an inlet-type boundary con-dition,since there isflow into the computational domain. However,the boundary condition has to be carefully set, based on the given constraints and the localflow-field conditions.In this study,we specify the massflow rate,total enthalpy and static pressure of the inlet.In addition, the turbulence level and the turbulent viscosity are specified for the model.The turbulent viscosity is needed only for the specification of the dissipation of turbulent kinetic energy at the inlet.In the present case,the local velocity is used as the reference velocity for turbulence level.Naturally,the mass fractions of the species are also specified.For a subsonic inlet,the static pressure is extrapo-lated from theflowfield,whereas in a supersonic inlet, all the conditions should be set from the inlet side.In practice,the inlet pressure is limited from below with a sonic pressure based on the given and.For more details,see Kaurinkoski.122.7Solution AlgorithmThe discretized equations are integrated in pseudo-time applying the factorization.13This is based on the approximate factorization and on the splitting of the Jacobians of theflux terms.The resulting implicit stage consists of a backward and forward sweep in every co-ordinate direction.The sweeps are based on afirst-order upwind differencing.In addition,the linearization of the source term is factored out of the spatial sweeps.The boundary conditions are treated explicitly,and a spatiallyvarying time step is utilized.The implicit stage can be written after factorization as follows(24) where is an identity matrix,and arefirst-order spatial difference operators in the,and direc-tions,,and are the corresponding Jacobian ma-trices,,and is the right-hand side ofEq.(18).The Jacobians are calculated as(25) where are diagonal matrices containing the positiveand negative eigenvalues,and is a factor to ensure thestability of the viscous term.The idea of the diagonally dominant factorization is to put as much weight on thediagonal as possible.In the direction,as well as in the and directions,the tridiagonal equation set resulting from Eq.(24)is replaced by two bidiagonal sweeps anda matrix multiplication.In order to simplify the linearization of the source term ,the wall-reflection terms involving wall distances are not linearized.Also,for stability reasons,only negative source terms are linearized in the Jacobian matrix.In order to account for the positive source terms,the following trick is applied(26)In this way,the maximum change of caused byis limited to.The actual limit may be eval-uated in many ways.Currently,the contributions of are included in a very approximate fashion:The maxi-mum change of is limited with. For the equation,the term is linearized as,i.e.,is considered independent of.A further simplification is to utilize the trick suggested by Vandromme14(28)In order to accelerate convergence,a multigrid method is employed.The multigrid cycling employs a V cycle and is based on the method by Jameson.15The details of the implementation are found in Ref.162.8Equation of State for an ArbitraryMixture of GasesThe thermodynamic properties of a mixture of gases can be determined by analyzing the thermodynamics of the components of the mixture.Each component in turn is a thermally perfect gas and the difficulty of the whole problem is divided into smaller ones.For each species, we can write(29)(30)(31)(32) where is the partial pressure and is the specific gas constant of species.For a mixture of species we have(33)(34)(35)where(39)Eq.(38)can be written for each species of a mixture.For temperatures less than C,we may use C in order to obtain a continuous function for.Then we can write(40) where is the reference specific internal energy of species at ing Eq.(38),we obtain after integration the functional form of as(41) where(42) Throughout this work,the emphasis is to develop an equation of state with and as parameters.For a given mixture,a set of:s that is,Eq.(41)links with as .Solving for is the main problem here,since after that the calculation of is trivial.Unfortunately,the direct solution of from(41)is quite complicated,be-cause,in general,we cannot make any dramatic assump-tions concerning,,or.However,sufficient accuracy is obtained with a fourth-order Taylor polyno-mial,which is developed here.Define a function to be the inverse function of(41),i.e.(43) Then,an approximation for can be calculated from(45) Formally,is calculated from(47) where(48)on the base surface.The value in the centre of the first cell above the surfaces was kept below in all of the calculated cases.The grid around the Baseline projectile is seen in Fig.1,and Fig.2shows a close-up view of the grid near the base region of the Dome(left) and the Cavity geometries(right).The diameter of the base-bleed hole is m for the Baseline geome-try and m for the Dome and Cavity geometries, respectively.With all the geometries,the inlet hole was modelled with an patch on the base surface.4Computed CasesTwo Mach numbers are studied,and ,both with two massflow rates for the base bleed.The calculated cases are presented in Table1.The massflow rate is expressed with the non-dimensional quantity defined byA1450 B2370 C2370 D2370 Table2:The model parameters for Eq.(37)and composition of the gases referred to as Smoke and Air.Smoke 1.000031.273 4.4010.399-0.0002Fig.3:The pressure coefficient distributions(left)and the friction coefficient distributions(right)in case C.Fig.4:The pressure coefficient distributions on the base surface of the different projectiles in case A(left)and case B(right).Fig.5:The pressure coefficient distributions on the base surface of the different projectiles in case C(left)and case D(right).,which in turn is a function of the non-dimensionalmassflow rate and the free-stream Mach number.The base drag reduction coefficient due to base bleed isdefined byTable3:The drag coefficient of all the geometries in different cases.and.Baseline Dome Cavity A0.80B0.72C0.82D0.74and Cavity geometries the pressure over the jet hits the sonic pressure lower limit,and therefore the pressure is constant over the jet.For the Baseline geometry this does not happen.As expected,outside the jet,the pres-sure distributions for the Baseline and the Cavity geometries are very similar,but not identical.A common property of all the numerical results is an extremely high level of turbulent kinetic energy at the centres of the vortices behind the bases of the shells. This might have something to do with the excessive base drag,because withfixed total internal energy,increasing the turbulent kinetic energy reduces the specific internal energy,which also reduces pressure.Consequently the base drag increases.6ConclusionsTheflow past a supersonic projectile with base bleed has been simulated with various base geometries.Differ-ent free-stream and base-bleed boundary conditions were simulated in order to compare the properties of the differ-ent base geometries.The simulations tend to overpredict the base drag,and consequently the base-drag reduction coefficients are underpredicted.In spite of the uncertainties in turbulence modelling, the results are now already considered to be applicable for the comparison of different geometries.Future devel-opment includes modelling of the chemical reactions at the base jet and possibly more advanced turbulence mod-elling.It is felt that in the future the present simulation method will be a useful tool in the determination of the aerodynamic coefficients and in the design of advanced projectiles.The new thermodynamic model employed in this study does not seem to significantly affect the results.However,the ability to simulate theflow of an inhomo-geneous mixture is created,and altering the model for an individual species can be done rather quickly.7AcknowledgementsThis research project has been mainly funded by MA-TINE,the Scientific Commitee of National Defence, and MATLE,the Defence Materiel Establishment of the Finnish Defence Forces.Their support for this research is gratefully acknowledged.ReferencesArena,Jr.,A.S.,Nelson,R.C.,and Schiff,L.B.,“Directional Control at High Angles of Attack Us-ing Blowing Through a Chined Forebody,”Journal Of Aircraft,V ol.32,May-June1995,pp.596–602.Nusca,M.J.,“Numerical Simulation of Gas Dynam-ics and Combustion for120-mm Ram Accelerator,”in Proceedings of the14th International Symposium on Ballistics,V ol.1,(Québec),pp.261–272,Sep 1993.ISBN0–9618156–9–8.Sahu,J.,Nietubicz,C.J.,and Steger,J.L.,“Navier–Stokes Computations of Projectile Base Flow with and without Mass Injection,”AIAA Journal,V ol.23, Sep1985,pp.1348–1355.Ju,Y.,“Lower–Upper Scheme for Chemically React-ing Flow with Finite Rate Chemistry,”AIAA Journal, V ol.33,Aug1995,pp.1418–1425.Palmer,G.and Venkatapathy, E.,“Comparison of Nonequilibrium Solution Algorithms Applied to Chemically Stiff Hypersonic Flows,”AIAA Journal, V ol.33,Jul1995,pp.1211–1219.Kaurinkoski,P.,Salminen, E.,and Siikonen,T.,“Computation of Turbulent Flow over Finned Projec-tiles,”in1994AIAA Atmospheric Flight Mechanics Conference,(Scottsdale,Arizona),pp.378–387,Aug 1994.AIAA Paper94-3502-CP.Anderson,Jr.,J.D.,Hypersonic and High Tempera-ture Gas Dynamics.New York:McGraw–Hill Book Co.,1989.ISBN0–07–001671–2.Chien,K.-Y.,“Predictions of Channel and Boundary-Layer Flows with a Low-Reynods-Number Turbu-lence Model,”AIAA Journal,V ol.20,Jan1982, pp.33–38.Menter,F.R.,“Zonal Two Equation Turbulence Models for Aerodynamic Flows,”in24th AIAA Fluid Dynamics Conference,(Orlando,Florida),Jul1993. AIAA Paper93-2906-CP.Siikonen,T.,“An Application of Roe’s Flux Dif-ference Splitting for the Turbulence Model,”Helsinki University of Technology,Laboratory of Aerodynamics,1994.ISBN951–22–2059–8.Roe,P.,“Approximate Riemann Solvers,Parameter Vectors,and Difference Schemes,”Journal of Com-putational Physics,V ol.43,1981,pp.357–372.Kaurinkoski,P.,Numerical Determination of the Flow of an Arbitrary Mixture of Gases.Licentiate’s thesis,Helsinki University of Technology,Dec1995. Lombard, C.,Bardina,J.,Venkatapathy, E.,and Oliger,J.,“Multi-Dimensional Formulation of CSCM—An Upwind Flux Difference Eigenvec-tor Split Method for the Compressible Navier–Stokes Equations,”in6th AIAA Computational Fluid Dynamics Conference,(Danvers,Massachusetts), pp.649–664,Jul1983.AIAA Paper83-1895-CP. Vandromme,D.,“Turbulence Modeling for Turbu-lent Flows and Implementation in Navier–Stokes Solvers,”in Introduction to the Modeling of Turbu-lence,von Karman Institute for Fluid Dynamics Lec-ture Series1991-02,1991.Jameson,A.and Yoon,S.,“Multigrid Solution of the Euler Equations Using Implicit Schemes,”AIAA Journal,V ol.24,No.11,1986.Siikonen,T.,Hoffren,J.,and Laine,S.,“A Multigrid Factorization Scheme for the Thin-Layer Navier–Stokes Equations,”in Proceedings of the17th ICAS Congress,(Stockholm),pp.2023–2034,Sep1990. ICAS Paper90-6.10.3.Knacke,O.,Kubaschewski,O.,and Hesselmann,K., Thermochemical Properties of Inorganic Substances. Berlin:Springer-Verlag,2nd ed.,1991.ISBN3–540–54014–8.White, F.M.,Viscous Fluid Flow.New York: McGraw–Hill Book Co.,2nd ed.,1991.ISBN0–07–069712–4.Vähäkangas,P.and Heininen,T.,“PVY-ruudin palolämpötilan laskennallinen määrittäminen,”Puo-lustusvoimien Tutkimuskeskus,Lakiala,Mar1993. (In Finnish,unpublished).Gunners,N.-E.,Andersson,K.,and Hellgren,R.,“Base–Bleed Systems for Gun Projectiles,”AIAA Progress in Astronautics and Aeronautics,V ol.109, 1988,pp.537–562.。
TSI AeroTrak+ 迷你级别粒子计数器 A100 系列应用文档 CC-120(A4)版本B说
Sampling Compressed Gases Using the TSI AeroTrak ™+ Portable Particle Counter A100 SeriesApplication Note CC-120 (A4)Rev B IntroductionCompressed air is used abundantly inpharmaceutical and electronics cleanrooms.Some uses of compressed gases includede-dusting, spray-coating tablets, over-pressurizing mixing and holding tanks,driving liquids through fill lines and filters,and operating control valves. However,compressed gases can be a source ofcontamination if not sufficiently clean.Leading facilities will therefore routinely testtheir compressed gases.Measuring the cleanliness of compressedgas is challenging. The high pressure of acompressed gas system can overwhelm aparticle counter, forcing more air throughthe particle counter than it was designedfor. The higher flow rate will cause errors inthe particle measurements and could evendamage the particle counter. Gases alsohave different densities, but particlecounters are generally calibrated for sampling air. This results in an inaccurate result because, unless corrected for, the sample volume is incorrect.To obtain accurate particle counts for a compressed gas requires two considerations:•Reducing the flow rate using a high-pressure diffuser •Correcting for the specific gravity of the gas being sampledSelecting a High Pressure DiffuserGas pressures above ambient room pressure require theuse of pressure-reducing equipment specificallydesigned for particle counting applications. TSI HighPressure Diffusers (HPDs) allow sampling with a particlecounter of non-reactive gas with pressures up to 120 PSI(8.3 bar) without introducing contaminants into thesample.There are two TSI HPD models that can be used with theAeroTrak+ Portable Particle Counter A100 Series. TheModel 7960 HPD is suitable for use for most gases,being used with sample flow rates of 1 CFM, 50 LPMand 100 LPM.However, for sampling very low humidity gases used inelectronic manufacturing, the TSI Model 7955 HPD mustbe used. This is because extremely dry air can abradethe fan and optics of the particle counter. The Model 7955 HPD uses HEPA-filtered room air to add moisture to the sampled air to allow the air to flow smoothly, without damaging the particle counter. It can only be used with a sample flow rate of 1 CFM.Correcting for Specific GravityParticle counters are calibrated to measure volumetric flow based on a specific gas, normally air. If other gases are sampled, the results will not reflect the programmed sample volume because of varying gas densities. Specific gravity, also known as relative density, of gases is defined as the ratio of the density of the gas to the density of the air at a specified temperature and pressure.Specific Gravity can be calculated asSG = ρgas/ ρairwhereSG = specific gravity of gasρgas = density of gas [kg/m3]ρair = density of air (normally at NTP - 1.204 [kg/m3])NTP - Normal Temperature and Pressure - defined as 20oC (293.15 K, 68oF) and1 atm (101.325 kN/m2, 101.325 kPa, 14.7 psia, 0 psig, 30 in Hg, 760 torr)Molecular weights can be used to calculate specific gravity if the densities of the gas and the air are evaluated at the same pressure and temperature.(Source: https:///density-specific-weight-gravity-d_290.html)Depending on the flow control method of the particle counter, a gas sample other than air can be normalized to the correct result for the actual sample volume desired by use of a correction factor based on specific gravity. For example, a 1 cubic foot sample result for nitrogen taken in a particle counter calibrated for air would have to be multiplied by 0.972 to obtain the equivalent result if an actual cubic foot of nitrogen is sampled. Because the particle counter is flow calibrated to the density of air, it would actually be taking a slightly larger sample of nitrogen because of the lower density of nitrogen.Other gases have similar correction factors, some larger or smaller, depending on the actual gas density. The AeroTrak+ Portable Particle Counter A100 Series can automatically apply the applicable correction factor for the gases listed in Table 1.Table 1: Gas Specific GravityAir 1Argon (Ar) 1.379Carbon Dioxide (CO2) 1.519Nitrogen (N2) 0.972To apply the correction factor, simply select the appropriate Sample Gas from the Sample Parameters dropdown menu in the Manual Mode Quick Settings or Monitor Zone creation screens. The selected sample volume is automatically programmed for the selected gas and results are corrected to obtain and accurate result.Figure 1 — Selecting a Sample Gas on the Sampling Parameters Screen_____________________ TSI and the TSI logo are registered trademarks of TSI Incorporated in the United States and may be protected under other country’s trademark registrations. TSI Incorporated – Visit our website for more information.USATel: +1 800 680 1220 UKTel: +44 149 4 459200 FranceTel: +33 4 91 11 87 64 GermanyTel: +49 241 523030 India Tel: +91 80 67877200 China Tel: +86 10 8251 6588 Singapore Tel: +65 6595 6388 CC-120 Rev B (4/25/2023) A4 ©2023 TSI Incorporated Printed in U.S.AEvaluating Results and Industry StandardsLife Sciences and other established cleanroom manufacturing operators typically use cleanroomstandards, notably ISO 14644-1, as guidelines for compressed air and gas particulate levels. SEMI E49 contains material pertinent to the electronics/semiconductor industry. ISO 8573 addresses compressed air (but not any other gas) limits and procedures for various types of contamination. The particulate limits for compressed gases in ISO 8573-1:2010 differ from the particulate limits for cleanrooms from ISO 14644-1:2015.Cleanroom personnel should determine the appropriate particulate contamination limits of compressed air or gas used in a cleanroom based on established risk assessment tools for the process taking place in the cleanroom. Specifying compressed air to be cleaner than the surrounding clean space may not be cost-effective, whereas specifying insufficiently clean air may introduce contamination. Forpharmaceutical applications, the US Food and Drug Administration requires compressed gases to be at least as clean as the area into which the gases are introduced.。
Towards sustainable and versatile energy storage devices
Received 1st March 2013 Accepted 8th May 2013 DOI: 10.1039/c3ee40709h /ees
Broader context
State-of-the-art Li-ion batteries recently met their development bottleneck because of the energy-density limitation of inorganic intercalation cathodes, in addition to the resources and environmental issues brought about by large-scale use of transitional metal based electrode materials. As an alternative, organic electrode materials have attracted more-and-more interest in recent years due to their high electrochemical performance, resource sustainability, environmental friendliness, structure diversity, exibility and so on. Since 1969, a many organic electrode materials with various structures have been investigated as cathodes or anodes for various energy storage devices including Li–organic batteries. The previous researches indicate that conducting polymers, nitroxyl radical polymers and conjugated carbonyl compounds are promising organic electrode candidates for the next generation of cheap, green, sustainable and versatile energy storage devices beyond conventional Li-ion batteries.
The Magnetic Origin of the Coherent Order Parameter in Hole-Doped Cuprates
c o nd -m a t /9905308 v 5 16 J u l 1999The Magnetic Origin of the Coherent Order Parameter in Hole-Doped CupratesA. Mourachki neUniversité Libre de Bruxelles, Service de Physique des Solides, CP233, Boulevard du Triomphe, B-1050 Brussels, Belgium ____________________________________________________________________________AbstractThe phase di agram for hole-doped cuprates is di scussed. By examining some recent inelastic neutron scattering data obtained on hole-doped cuprates we conclude that the coherent gap in hole-doped cuprates has most likely the magnetic origin and scales with T c , on average, as 2∆c /k B T c = 5.4.Keywords : A. High-T c superconducti vi ty __________________________________________________________________1. Introduction The superconductivity requires the formation of the Cooper pairs and the phase coherence among them. In the BCS theory for conventional superconductors, the mechani sms responsi ble for the pai ri ng and establishment of the phase coherence are identical: electrons couple to each other by phonons,and the phase coherence among the Cooper pairs is established also by phonons.Both phenomena occur almost si multaneously at T c . In superconducti ng copper-oxides (high-T c superconductivity), there is a consensus that these twomechanisms occur at different temperatures, at least, in the underdoped regi me,T pai r ≥ T c [1-6]. The order parameters (OPs) responsible for each process have different dependencies on hole concentrati on, p in CuO 2 planes [1,2]. The magnitude of the OP responsible for phase coherence, ∆c , which is proportional to T c , has the parabolic dependence on p [1,2,6,7]. While the magni tude of the OP responsible for pai ri ng, ∆p , i ncreases linearly with the decrease of hole concentration [1,2,8]. Both the ∆c and ∆p OPs are superconducti ng-li ke. However,there is no consensus on the origins of the two OPs. There is an evidence that the spi n-exchange interactions play a central role in the cuprates [9,10]. Thus, it is reasonable to assume that one out of the two OPs has the magnetic origin.Recent inelastic neutron scattering (INS) experi ments have shown the presence of sharp magneti c collective mode ('resonance peak') in thesuperconducti ng state of YBa2Cu3O6+x(YBCO) [10-15]. The discovery of the resonance peak in Bi2Sr2CaCu2O8+x(Bi2212) [16] points out that the resonance peak is an intrinsic feature of the superconductivity in the double-layer cuprates studied so far. The temperature dependence of the resonance peak demonstrates that this peak is intimately related to the establishment of superconductivity [17,10]. It is important to note that the E r is in quantitative agreement with the condensation energy of YBCO [18,19,10]. The resonance peak has been also observed by INS in a heavy fermi on compound UPd2Al3[20,21] for whi ch spi n fluctuations are believed to mediate the pai ri ng interactions [22,23]. It is also important to note that the superconductivity in UPd2Al3coexists with the anti ferromagneti c order like in the cuprates. By maki ng a parallel between the cuprates and heavy fermi on compound UPd2Al3, the latter suggests that, in the hole-doped cuprates, there is an OP having the magnetic origin.In the present work, we discuss the phase di agram and INS data obtained on hole-doped cuprates, and we conclude that the coherent OP, ∆c, has most likely the magneti c ori gi n.2. The coherent OP and INS dataFigure 1 shows a phase di agram for two energy gaps [24] in hole-doped cuprates [1,2]. In Fig. 1, the coherent gap, ∆c, scales with T c as 2∆c/k B T c= 5.45 [1,2]. The dependence ∆c(p) is parabolic since T c= T c, max[1 - 82.6(p - 0.16)2], where T c, max is the maxi mum T c for each family of cuprates [7]. In Fig. 1, we present also INS data for YBCO [10-15] and Bi2212 [16], which can be found in Table I. One can see in Fig. 1 that there is a good agreement between the ∆c and the INS data. So, it is reasonable to assume that the ∆c has the magnetic origin.In general, the superconductivity mediated by spin fluctuations implies that the coherent gap in hole-doped cuprates has the d x2- y2 symmetry [9]. The average 2∆c/k B T c value for the data presented in Table I is equal to 5.38.3. DiscussionIn UPd2Al3, the resonance-peak position E r= 0.36 meV [20] does not match exactly the value of tunneli ng gap 2∆= 0.47 meV [22] like it is in Fig. 1 for cuprates. There are, at least, two reasons for this. First of all, the INS measurements have been performed on UPd2Al3single crystals whereas the tunneli ng measurements on thin films [20,22]. The second and, maybe, the mostimportant reason for the small di screpancy between the tunneli ng and INS data is an anisotropic character of the energy gap whi ch has most likely the d-wave symmetry [22,9]. The resonance peak in UPd2Al3is detected at the anti fferomagneti c Bragg point (0, 0, 0.5) [20], while the tunneli ng spectra are measured along the c-axis [22]. Thus, the INS and tunneli ng data obtained at different angles on the Fermi surface, and it is the mai n reason for the discrepancy of the data since the energy gap is anisotropic (d-wave).The quasiparticles in conventional superconductors use phonons for pairing. Most likely, INS detects spin fluctuations whi ch replace phonons [9]. Another explanation for the presence of the resonance peak in hole-doped cuprates is that it corresponds to the response of the magnetic domains in CuO2 planes to the hole pairing [25]. It may be the case. However, the same response has been detected in the heavy fermion compound UPd2Al3 in which the superconductivity is mediated by spin fluctuations [22,23]. Thus, in both cases, this is an evidence for the presence of the magnetically-mediated superconductivity in hole-doped cuprates.In order to explain the data, recently, we proposed a MCS (Magnetic Coupli ng of Stripes) model [6,2] which is based on the stripe model [26] whi ch is in it's turn based on a spinon superconductivity along charge stripes. The mai n di fference between the MCS and stripe models is that the coherent state of spinon superconductivity is established differently in the two models, by spin fluctuations into anti ferromagneti c domai ns of CuO2planes in the MCS model, and by the Josephson coupling between stripes in the stripe model. Thus, in the MCS model, the superconductivity has two different mechani sms: along charge stripes for pai ri ng and perpendi cular to stripes for establishing the coherent state. As a consequence, carri ers exhibit different properties in different directions: fermionic along charge stripes and polaronic perpendi cular to stripes. We found that many experimental data can be explained by the MCS model [27]. Moreover, the MCS model may explain the s-wave superconductivity [28] in an electron-doped Nd2-x Ce x Cu2O4 cuprate [6,27]. However, it is possible that there is another model of high-T c superconductivity whi ch can explain experi mental data better. Unfortunately, we are not aware of such model.4. ConclusionsWe di scussed the phase di agram for the phase-coherence and pai ri ng order parameters in hole-doped cuprates. By exami ni ng some recent inelastic neutron scattering data obtained on hole-doped cuprates we concluded that the coherentorder parameter has most likely the magneti c origin and scales with T c, on average, as 2∆c/k B T c= 5.4. We di scussed also the MCS model of high-T c superconductivity in hole-doped cuprates.AcknowledgmentsI thank R. Deltour for a discussion. This work is supported by PAI 4/10. References[1] G. Deutscher, Nature 397 (1999) 410.[2] A. Mourachkine, cond-mat/9811284 and cond-mat/9812245.[3] J. Corson, R. Mallozzi, J. Orenstein, J.N. Eckstein, and I. Bozovic, Nature398 (1999) 221.[4] A. Mourachkine, cond-mat/9903395.[5] Ch. Renner, B. Revaz, J.-Y. Genoud, K. Kadowaki, and Ø. Fi cher, Phys.Rev. Lett. 80 (1998) 149.[6] A. Mourachki ne, J. of Superconductivity, to be published, also cond-mat/9902355.[7] J. L. Tallon et al., Phys. Rev. Lett. 75 (1995) 3524.[8] N. Miyakawa, P. Guptasarma, J.F. Zasadzi nski, D.G. Hinks, and K.E. Gray,Phys. Rev. Lett. 80 (1998) 157; and cond-mat/9809398.[9] D. J. Scalapino, Science 284 (1999) 1282.[10] P. Dai et al., Science 284 (1999) 1344.[11] H. F. Fong et al., Phys. Rev. Lett. 78 (1997) 713.[12] P. Dai, H. A. Mook and F. Dogan, Phys. Rev. Lett. 80 (1998) 1738.[13] L. P. Regnault et al., Physica C 235-240 (1994) 59.[14] P. Bourges et al., Phys. Rev. B 53 (1996) 876.[15] H. A. Mook et al., Phys. Rev. Lett. 70 (1993) 3490.[16] H. F. Fong et al., Nature 398 (1999) 588.[17] P. Bourges, In The gap symmetry and fluctuations in high temperaturesuperconductors, edited by J. Bok et al., Plenum press, 1998.[18] D. J. Scalapino and S. R. White, Phys. Rev. B 58 (1998) 8222.[19] E. Demler and S.-C. Zhang, Nature 396 (1998) 733.[20] N. Metoki et al., Phys. Rev. Lett. 80 (1998) 5417.[21] S. Hayden, Physics World, 18 (February 1999).[22] M. Jourdan, M. Huth and H. Adrian, Nature 398 (1999) 47.[23] N. D. Marthur et al., Nature 394 (1998) 39.[24] In this paper, the two terms “energy gap” and “order parameter” will be usedwithout distinction.[25] J. M. Tranquada, cond-mat/9903458.[26] V. J. Emery, S. A. Kivelson, and O. Zachar, Phys. Rev. B 56 (1997) 6120.[27] A. Mourachkine, J. of Superconductivity, to be published, also cond-mat/9904445.[28] S. M. Anlage, D.-H. Wu, J. Mao, S. N. Mao, X. X. Xi, T. Vankatesan, J. L.Peng, and R. L. Greene, Phys. Rev. B 50 (1994) 523.Table I INS data presented in Fig. 1YBCO6+x Tc(K)Er(meV) Er/ kBTcRef.x = 0.55225 5.6110.662.734 6.3120.76733 5.72110.88239 5.53100.838535 4.8130.929141 5.24130.9792.540 5.0314192.441 5.161519341 5.131118939 5.113 Bi22129143 5.516FIG. 1. Phase diagram for hole-doped cuprates: ∆c is the coherent energy gap and ∆p is the pai ri ng energy gap [1]. INS data: dots (YBCO) and square (Bi2212). For detailed references, see Table I. The p m is a hole concentration with the maxi mum T c.。
湍流燃烧模型
Contents
1. Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 195 2. Balance equations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 196
194
D. Veynante, L. Vervisch / Progress in Energy and Combustion Science 28 (2002) 193±266
6. Tools for turbulent combustion modeling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 212 6.1. Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 212 6.2. Scalar dissipation rate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 214 6.3. Geometrical description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 214 6.3.1. G-®eld equation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 214 6.3.2. Flame surface density description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 216 6.3.3. Flame wrinkling description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 218 6.4. Statistical approaches: probability density function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 218 6.4.1. Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 218 6.4.2. Presumed probability density functions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 219 6.4.3. Pdf balance equation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 219 6.4.4. Joint velocity/concentrations pdf . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 221 6.4.5. Conditional moment closure (CMC) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 221 6.5. Similarities and links between the tools . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 221
安东尼·巴尔低温粘度测量仪说明书
Low Temperature Viscosity Measurements -Lovis for Battery ElectrolytesRelevant for: battery industry, electrochemical research, automotive industryPerform viscosity measurements down to -20 °C with Lovis 2000 M/ME with cooling option. Test even highly corrosive solvents for ion salts by using unbreakable PCTFE capillaries with small filling volumes (110 µL or 450 µL). Handling of the sample inside a glove box filled with inert gas and a hermetically closed system prevent contamination or evaporation of the sample.1 IntroductionSince the introduction of the lithium-ion batteries in 1990, the interest in this technology has emerged steadily, not only for portable devices but also for the automotive industry. Their high energy density as well as outstanding cycle stability are the main reasons for commercial success, but several problems arise with the usage of the most common non-aqueous electrolytes, which contain lithiumhexafluoro-phosphate (LiPF6) as conductive salt and a mixture of cyclic and non-cyclic organic carbonates.In addition to the high purity required of all used solvents (e.g. traces of protic impurities such as water can cause severe deterioration of the cell performance after a short life / cycle time) the cell performance has to be stable over a broad temperature range from arctic to tropical conditions without any significant degradation. Therefore, an exact characterization of newly developed electrolytes at different temperatures is an essential part in the lithium-ion cell research today. These challenges have to be considered for every other upcoming battery systems like magnesium ion cells or sulfur cells, too.Therefore, research companies use different standard electrochemical measurements for monitoring batteries. In this connection viscosity, conductivity and – if required – density measurements of the electrolytes support those investigations.The performance of the charge and discharge rate of a rechargeable battery, that is the ion transport, is characterized by the ion conductivity, which depends on the viscosity and the dielectric constant.The viscosity of the solvent, in which the ion salt is solved, affects the mobility of ions, as shown in the Stokes-Einstein equation; mobility is inversely proportional to the viscosity:r ... radius of the solvated ionBased on those viscosity measurements important conclusions on the wettability of the electrode /electro-lyte interface can be drawn, too. Fast, accurate and reproducible viscosity measurement over a wide temperature range is highly desirable for successful development of new electrolyte systems.This application report shows how the Lovis can be used for electrolyte measurements even at tempera-tures below zero. The Lovis, equipped with coolingoption and in combination with the capillary made of PCTFE, enables measurement of highly corrosive substances over a wide temperature range.2 Instrumentation2.1Lovis 2000 M/ME Microviscometer with Cooling OptionFigure 1: Lovis 2000 M with cooling optionThe Lovis 2000 M/ME Microviscometer measures the rolling time of a ball inside an inclined capillary.Variable inclination angles allow for measurements at different shear rates. Temperature control via Peltier elements is extremely fast and provides utmost accuracy.For measuring at temperatures below zero, the Lovis ME Module can be equipped with a lowtemperature option. In combination with a recirculating cooler, it is possible to measure at temperatures as low as -20 °C (lower temperatures down to -30 °C on request, depending on the cooling liquid of the recirculating cooling, ambient temperature and ambient air humidity).The integrated software calculates the kinematic or dynamic viscosity, provided the sample's density value is known.Figure 2: Lovis PCTFE capillariesWith the PCTFE capillaries it is possible to measure nearly every liquid, also corrosive, aggressive or hazardous solvents and electrolytes.The measuring viscosity of a PCTFE capillary ranges from 0.8 mPa.s to 160 mPa.s.Used material:▪ Capillary: PCTFE short (110 µL) ▪ Capillary diameter: 1.62mm ▪ Ball material: Steel ▪ Ball diameter: 1.5 mm2.3 Additional Equipment▪ Glove box filled with argon.▪Circulation cooler plus insulated hoses. How to set up the cooling is precisely described in the documentation of Lovis 2000 M/ME.3MeasurementAll determinations were performed manually without autosampler. The viscosity measurements were performed in a temperature range from -20 °C to +60 °C with steps of 5 °C or 10 °. For temperature table scans (TTS) two density values at two different reference temperatures were typed in manually in the "Quick Settings" ("Lovis Density TS/TTS") for every sample. The instrument automatically extrapolated the missing temperature / density values by linearextrapolation. The density values for the manual input were determined with the SVM™.Every scan was performed twice in order to obtain a repeat determination. To check the reproducibility, all measurements were performed with Lovis and SVM™ in parallel.3.1 Samples▪Different mixtures of organic carbonates, which contain lithiumhexafluorophosphate as conductive salt – for lithium ion batteries (LIB), either commercial available standardelectrolytes or newly developed electrolyte solutions.▪Solvents containing a polar organic solvent and dioxolane added with Li-sulfur-compounds as conductive salts – for future Li-S-cell systems (LiS).▪Solvents containing a polar organic solvent plus Mg-compounds as conductive salts – for prospective Mg-ion batteries.3.2 Instrument Settings Measuring Method: Temperature Table Scan (TTS) Measuring Settings:▪ Temperature: scan between -20 °C to +60 °C ▪ Equilibration Time: no ▪ Measurement Cycles: 3▪ Measuring Angle: Auto Angle * ▪ Variation Coefficient:0.4 % for standard electrolytes ▪ Measuring Distance: Short* Adjustment was performed over an angle range from of 20° to 70° in 10° steps3.3 Filling of the CapillaryAll samples were manually filled in an argon glove box under inert conditions. For each measurement a new steel ball was used to avoid any cross contamination from one measurement to the other. After closing the capillary with the appropriate plug, the hermetically sealed capillary was removed from the glove box.3.4 CleaningThe capillary was cleaned thoroughly with smallbrushes after every test sequence. Ethanol, deionized water and other appropriate solvents were used as cleaning liquids. If necessary, the capillary was placed into an ultrasonic bath (approximately 10 to 20 min, 30 °C, water plus standard detergent). Afterwards the capillary was dried under a pressure-less nitrogen stream.4 ResultsFigure 3: Reproducibility check; standard Li-ion electrolyte V24 measured with Lovis and SVM ™ from +20 °C to -20 °C4.4Temperature Profile of Li-polysulfide4.5Checking the Influence of Conducting Salt5ConclusionBy using the Lovis 2000 M/ME equipped with cooling option, it is possible to perform measurements from -20 °C up to +100 °C. In combination with the capillary made of PCTFE even extremely corrosive substances can be measured under hermetically sealed atmosphere. This allows users to measure theviscosity of electrolytes, which might be destroyed or changed in structure by air and/or air humidity.▪ The small capillary sizes require only littlesample volume (starting from 110 µL). ▪ The small diameter of the PCTFE capillary(1.62 mm) enables also the measurement of very low-viscosity samples (viscosity range from 0.8 mPa.s to 160 mPa.s).▪ The cooling option allows for viscositymeasurements down to -20 °C (lowertemperatures down to -30 °C are possible on request and depending on ambient conditions).▪ The closed system avoids any contaminationand evaporation.▪ The variable inclination angle of themeasurement allows for the variation of the shear rate.▪ Lovis 2000 M/ME is highly modular; it can becombined with DMA™ M Density Meters for automated calculation of dynamic andkinematic viscosity. It can also be combined with an Xsample™ sample changer (see Figure 8) for automatic filling and cleaning of the capillary and measurements with high sample throughput.6ReferencesSpecial thanks to DI Gisela Fauler and Ms. Katja Kapper from VARTA Micro Innovation GmbH who tested the Lovis with cooling option and the PCTFE capillaries and supported Anton Paar with their measurement data.Contact Anton Paar GmbH Tel: +43 316 257-0****************************|。
pwscf说明书
User’s Guide for Quantum ESPRESSO(version4.2.0)Contents1Introduction31.1What can Quantum ESPRESSO do (4)1.2People (6)1.3Contacts (8)1.4Terms of use (9)2Installation92.1Download (9)2.2Prerequisites (10)2.3configure (11)2.3.1Manual configuration (13)2.4Libraries (13)2.4.1If optimized libraries are not found (14)2.5Compilation (15)2.6Running examples (17)2.7Installation tricks and problems (19)2.7.1All architectures (19)2.7.2Cray XT machines (19)2.7.3IBM AIX (20)2.7.4Linux PC (20)2.7.5Linux PC clusters with MPI (22)2.7.6Intel Mac OS X (23)2.7.7SGI,Alpha (24)3Parallelism253.1Understanding Parallelism (25)3.2Running on parallel machines (25)3.3Parallelization levels (26)3.3.1Understanding parallel I/O (28)3.4Tricks and problems (29)4Using Quantum ESPRESSO314.1Input data (31)4.2Datafiles (32)4.3Format of arrays containing charge density,potential,etc (32)5Using PWscf335.1Electronic structure calculations (33)5.2Optimization and dynamics (35)5.3Nudged Elastic Band calculation (35)6Phonon calculations376.1Single-q calculation (37)6.2Calculation of interatomic force constants in real space (37)6.3Calculation of electron-phonon interaction coefficients (38)6.4Distributed Phonon calculations (38)7Post-processing397.1Plotting selected quantities (39)7.2Band structure,Fermi surface (39)7.3Projection over atomic states,DOS (39)7.4Wannier functions (40)7.5Other tools (40)8Using CP408.1Reaching the electronic ground state (42)8.2Relax the system (43)8.3CP dynamics (45)8.4Advanced usage (47)8.4.1Self-interaction Correction (47)8.4.2ensemble-DFT (48)8.4.3Treatment of USPPs (50)9Performances519.1Execution time (51)9.2Memory requirements (52)9.3File space requirements (52)9.4Parallelization issues (52)10Troubleshooting5410.1pw.x problems (54)10.2PostProc (61)10.3ph.x errors (62)11Frequently Asked Questions(F AQ)6311.1General (63)11.2Installation (63)11.3Pseudopotentials (64)11.4Input data (65)11.5Parallel execution (66)11.6Frequent errors during execution (66)11.7Self Consistency (67)11.8Phonons (69)1IntroductionThis guide covers the installation and usage of Quantum ESPRESSO(opEn-Source Package for Research in Electronic Structure,Simulation,and Optimization),version4.2.0.The Quantum ESPRESSO distribution contains the following core packages for the cal-culation of electronic-structure properties within Density-Functional Theory(DFT),using a Plane-Wave(PW)basis set and pseudopotentials(PP):•PWscf(Plane-Wave Self-Consistent Field).•CP(Car-Parrinello).It also includes the following more specialized packages:•PHonon:phonons with Density-Functional Perturbation Theory.•PostProc:various utilities for data postprocessing.•PWcond:ballistic conductance.•GIPAW(Gauge-Independent Projector Augmented Waves):EPR g-tensor and NMR chem-ical shifts.•XSPECTRA:K-edge X-ray adsorption spectra.•vdW:(experimental)dynamic polarizability.•GWW:(experimental)GW calculation using Wannier functions.The following auxiliary codes are included as well:•PWgui:a Graphical User Interface,producing input datafiles for PWscf.•atomic:a program for atomic calculations and generation of pseudopotentials.•QHA:utilities for the calculation of projected density of states(PDOS)and of the free energy in the Quasi-Harmonic Approximation(to be used in conjunction with PHonon).•PlotPhon:phonon dispersion plotting utility(to be used in conjunction with PHonon).A copy of required external libraries are included:•iotk:an Input-Output ToolKit.•PMG:Multigrid solver for Poisson equation.•BLAS and LAPACKFinally,several additional packages that exploit data produced by Quantum ESPRESSO can be installed as plug-ins:•Wannier90:maximally localized Wannier functions(/),writ-ten by A.Mostofi,J.Yates,Y.-S Lee.•WanT:quantum transport properties with Wannier functions.•YAMBO:optical excitations with Many-Body Perturbation Theory.This guide documents PWscf,CP,PHonon,PostProc.The remaining packages have separate documentation.The Quantum ESPRESSO codes work on many different types of Unix machines,in-cluding parallel machines using both OpenMP and MPI(Message Passing Interface).Running Quantum ESPRESSO on Mac OS X and MS-Windows is also possible:see section2.2.Further documentation,beyond what is provided in this guide,can be found in:•the pw forum mailing list(pw forum@).You can subscribe to this list,browse and search its archives(links in /contacts.php).Only subscribed users can post.Please search the archives before posting:your question may have already been answered.•the Doc/directory of the Quantum ESPRESSO distribution,containing a detailed de-scription of input data for most codes infiles INPUT*.txt and INPUT*.html,plus and a few additional pdf documents;people who want to contribute to Quantum ESPRESSO should read the Developer Manual,developer man.pdf.•the Quantum ESPRESSO Wiki:/wiki/index.php/Main Page.This guide does not explain solid state physics and its computational methods.If you want to learn that,you should read a good textbook,such as e.g.the book by Richard Martin: Electronic Structure:Basic Theory and Practical Methods,Cambridge University Press(2004). See also the Reference Paper section in the Wiki.This guide assume that you know the basic Unix concepts(shell,execution path,directories etc.)and utilities.If you don’t,you will have a hard time running Quantum ESPRESSO.All trademarks mentioned in this guide belong to their respective owners.1.1What can Quantum ESPRESSO doPWscf can currently perform the following kinds of calculations:•ground-state energy and one-electron(Kohn-Sham)orbitals;•atomic forces,stresses,and structural optimization;•molecular dynamics on the ground-state Born-Oppenheimer surface,also with variable cell;•Nudged Elastic Band(NEB)and Fourier String Method Dynamics(SMD)for energy barriers and reaction paths;•macroscopic polarization andfinite electricfields via the modern theory of polarization (Berry Phases).All of the above works for both insulators and metals,in any crystal structure,for many exchange-correlation(XC)functionals(including spin polarization,DFT+U,hybrid function-als),for norm-conserving(Hamann-Schluter-Chiang)PPs(NCPPs)in separable form or Ultra-soft(Vanderbilt)PPs(USPPs)or Projector Augmented Waves(PAW)method.Non-collinear magnetism and spin-orbit interactions are also implemented.An implementation offinite elec-tricfields with a sawtooth potential in a supercell is also available.PHonon can perform the following types of calculations:•phonon frequencies and eigenvectors at a generic wave vector,using Density-Functional Perturbation Theory;•effective charges and dielectric tensors;•electron-phonon interaction coefficients for metals;•interatomic force constants in real space;•third-order anharmonic phonon lifetimes;•Infrared and Raman(nonresonant)cross section.PHonon can be used whenever PWscf can be used,with the exceptions of DFT+U and hybrid functionals.PAW is not implemented for higher-order response calculations.Calculations,in the Quasi-Harmonic approximations,of the vibrational free energy can be performed using the QHA package.PostProc can perform the following types of calculations:•Scanning Tunneling Microscopy(STM)images;•plots of Electron Localization Functions(ELF);•Density of States(DOS)and Projected DOS(PDOS);•L¨o wdin charges;•planar and spherical averages;plus interfacing with a number of graphical utilities and with external codes.CP can perform Car-Parrinello molecular dynamics,including variable-cell dynamics.1.2PeopleIn the following,the cited affiliation is either the current one or the one where the last known contribution was done.The maintenance and further development of the Quantum ESPRESSO distribution is promoted by the DEMOCRITOS National Simulation Center of IOM-CNR under the coor-dination of Paolo Giannozzi(Univ.Udine,Italy)and Layla Martin-Samos(Democritos)with the strong support of the CINECA National Supercomputing Center in Bologna under the responsibility of Carlo Cavazzoni.The PWscf package(which included PHonon and PostProc in earlier releases)was origi-nally developed by Stefano Baroni,Stefano de Gironcoli,Andrea Dal Corso(SISSA),Paolo Giannozzi,and many others.We quote in particular:•Matteo Cococcioni(Univ.Minnesota)for DFT+U implementation;•David Vanderbilt’s group at Rutgers for Berry’s phase calculations;•Ralph Gebauer(ICTP,Trieste)and Adriano Mosca Conte(SISSA,Trieste)for noncolinear magnetism;•Andrea Dal Corso for spin-orbit interactions;•Carlo Sbraccia(Princeton)for NEB,Strings method,for improvements to structural optimization and to many other parts;•Paolo Umari(Democritos)forfinite electricfields;•Renata Wentzcovitch and collaborators(Univ.Minnesota)for variable-cell molecular dynamics;•Lorenzo Paulatto(Univ.Paris VI)for PAW implementation,built upon previous work by Guido Fratesi(ano Bicocca)and Riccardo Mazzarello(ETHZ-USI Lugano);•Ismaila Dabo(INRIA,Palaiseau)for electrostatics with free boundary conditions.For PHonon,we mention in particular:•Michele Lazzeri(Univ.Paris VI)for the2n+1code and Raman cross section calculation with2nd-order response;•Andrea Dal Corso for USPP,noncollinear,spin-orbit extensions to PHonon.For PostProc,we mention:•Andrea Benassi(SISSA)for the epsilon utility;•Norbert Nemec(U.Cambridge)for the pw2casino utility;•Dmitry Korotin(Inst.Met.Phys.Ekaterinburg)for the wannier ham utility.The CP package is based on the original code written by Roberto Car and Michele Parrinello. CP was developed by Alfredo Pasquarello(IRRMA,Lausanne),Kari Laasonen(Oulu),Andrea Trave,Roberto Car(Princeton),Nicola Marzari(Univ.Oxford),Paolo Giannozzi,and others. FPMD,later merged with CP,was developed by Carlo Cavazzoni,Gerardo Ballabio(CINECA), Sandro Scandolo(ICTP),Guido Chiarotti(SISSA),Paolo Focher,and others.We quote in particular:•Carlo Sbraccia(Princeton)for NEB;•Manu Sharma(Princeton)and Yudong Wu(Princeton)for maximally localized Wannier functions and dynamics with Wannier functions;•Paolo Umari(Democritos)forfinite electricfields and conjugate gradients;•Paolo Umari and Ismaila Dabo for ensemble-DFT;•Xiaofei Wang(Princeton)for META-GGA;•The Autopilot feature was implemented by Targacept,Inc.Other packages in Quantum ESPRESSO:•PWcond was written by Alexander Smogunov(SISSA)and Andrea Dal Corso.For an introduction,see http://people.sissa.it/~smogunov/PWCOND/pwcond.html•GIPAW()was written by Davide Ceresoli(MIT),Ari Seitsonen (Univ.Zurich),Uwe Gerstmann,Francesco Mauri(Univ.Paris VI).•PWgui was written by Anton Kokalj(IJS Ljubljana)and is based on his GUIB concept (http://www-k3.ijs.si/kokalj/guib/).•atomic was written by Andrea Dal Corso and it is the result of many additions to the original code by Paolo Giannozzi and others.Lorenzo Paulatto wrote the PAW extension.•iotk(http://www.s3.infm.it/iotk)was written by Giovanni Bussi(SISSA).•XSPECTRA was written by Matteo Calandra(Univ.Paris VI)and collaborators.•VdW was contributed by Huy-Viet Nguyen(SISSA).•GWW was written by Paolo Umari and Geoffrey Stenuit(Democritos).•QHA amd PlotPhon were contributed by Eyvaz Isaev(Moscow Steel and Alloy Inst.and Linkoping and Uppsala Univ.).Other relevant contributions to Quantum ESPRESSO:•Andrea Ferretti(MIT)contributed the qexml and sumpdos utility,helped withfile formats and with various problems;•Hannu-Pekka Komsa(CSEA/Lausanne)contributed the HSE functional;•Dispersions interaction in the framework of DFT-D were contributed by Daniel Forrer (Padua Univ.)and Michele Pavone(Naples Univ.Federico II);•Filippo Spiga(ano Bicocca)contributed the mixed MPI-OpenMP paralleliza-tion;•The initial BlueGene porting was done by Costas Bekas and Alessandro Curioni(IBM Zurich);•Gerardo Ballabio wrote thefirst configure for Quantum ESPRESSO•Audrius Alkauskas(IRRMA),Uli Aschauer(Princeton),Simon Binnie(Univ.College London),Guido Fratesi,Axel Kohlmeyer(UPenn),Konstantin Kudin(Princeton),Sergey Lisenkov(Univ.Arkansas),Nicolas Mounet(MIT),William Parker(Ohio State Univ), Guido Roma(CEA),Gabriele Sclauzero(SISSA),Sylvie Stucki(IRRMA),Pascal Thibaudeau (CEA),Vittorio Zecca,Federico Zipoli(Princeton)answered questions on the mailing list, found bugs,helped in porting to new architectures,wrote some code.An alphabetical list of further contributors includes:Dario Alf`e,Alain Allouche,Francesco Antoniella,Francesca Baletto,Mauro Boero,Nicola Bonini,Claudia Bungaro,Paolo Cazzato, Gabriele Cipriani,Jiayu Dai,Cesar Da Silva,Alberto Debernardi,Gernot Deinzer,Yves Ferro, Martin Hilgeman,Yosuke Kanai,Nicolas Lacorne,Stephane Lefranc,Kurt Maeder,Andrea Marini,Pasquale Pavone,Mickael Profeta,Kurt Stokbro,Paul Tangney,Antonio Tilocca,Jaro Tobik,Malgorzata Wierzbowska,Silviu Zilberman,and let us apologize to everybody we have forgotten.This guide was mostly written by Paolo Giannozzi.Gerardo Ballabio and Carlo Cavazzoni wrote the section on CP.1.3ContactsThe web site for Quantum ESPRESSO is /.Releases and patches can be downloaded from this site or following the links contained in it.The main entry point for developers is the QE-forge web site:/.The recommended place where to ask questions about installation and usage of Quantum ESPRESSO,and to report bugs,is the pw forum mailing list:pw forum@.Here you can receive news about Quantum ESPRESSO and obtain help from the developers and from knowledgeable users.You have to be subscribed in order to post to the list.Please browse or search the archive–links are available in the”Contacts”page of the Quantum ESPRESSO web site,/contacts.php–before posting: many questions are asked over and over again.NOTA BENE:only messages that appear to come from the registered user’s e-mail address,in its exact form,will be accepted.Messages”waiting for moderator approval”are automatically deleted with no further processing(sorry,too much spam).In case of trouble,carefully check that your return e-mail is the correct one(i.e.the one you used to subscribe).Since pw forum averages∼10message a day,an alternative low-traffic mailing list,pw users@,is provided for those interested only in Quantum ESPRESSO-related news,such as e.g.announcements of new versions,tutorials,etc..You can subscribe(but not post)to this list from the Quantum ESPRESSO web site.If you need to contact the developers for specific questions about coding,proposals,offersof help,etc.,send a message to the developers’mailing list:user q-e-developers,address.1.4Terms of useQuantum ESPRESSO is free software,released under the GNU General Public License. See /licenses/old-licenses/gpl-2.0.txt,or thefile License in the distribution).We shall greatly appreciate if scientific work done using this code will contain an explicit acknowledgment and the following reference:P.Giannozzi,S.Baroni,N.Bonini,M.Calandra,R.Car,C.Cavazzoni,D.Ceresoli,G.L.Chiarotti,M.Cococcioni,I.Dabo,A.Dal Corso,S.Fabris,G.Fratesi,S.deGironcoli,R.Gebauer,U.Gerstmann,C.Gougoussis,A.Kokalj,zzeri,L.Martin-Samos,N.Marzari,F.Mauri,R.Mazzarello,S.Paolini,A.Pasquarello,L.Paulatto, C.Sbraccia,S.Scandolo,G.Sclauzero, A.P.Seitsonen, A.Smo-gunov,P.Umari,R.M.Wentzcovitch,J.Phys.:Condens.Matter21,395502(2009),/abs/0906.2569Note the form Quantum ESPRESSO for textual citations of the code.Pseudopotentials should be cited as(for instance)[]We used the pseudopotentials C.pbe-rrjkus.UPF and O.pbe-vbc.UPF from.2Installation2.1DownloadPresently,Quantum ESPRESSO is only distributed in source form;some precompiled exe-cutables(binaryfiles)are provided only for PWgui.Stable releases of the Quantum ESPRESSO source package(current version is4.2.0)can be downloaded from this URL:/download.php.Uncompress and unpack the core distribution using the command:tar zxvf espresso-X.Y.Z.tar.gz(a hyphen before”zxvf”is optional)where X.Y.Z stands for the version number.If your version of tar doesn’t recognize the”z”flag:gunzip-c espresso-X.Y.Z.tar.gz|tar xvf-A directory espresso-X.Y.Z/will be created.Given the size of the complete distribution,you may need to download more packages and to unpack them following the same procedure(they will unpack into the same directory).Plug-ins should instead be downloaded into subdirectory plugin/archive but not unpacked or uncompressed:command make will take care of this during installation.Occasionally,patches for the current version,fixing some errors and bugs,may be distributed as a”diff”file.In order to install a patch(for instance):cd espresso-X.Y.Z/patch-p1</path/to/the/diff/file/patch-file.diffIf more than one patch is present,they should be applied in the correct order.Daily snapshots of the development version can be downloaded from the developers’site :follow the link”Quantum ESPRESSO”,then”SCM”.Beware:the develop-ment version is,well,under development:use at your own risk!The bravest may access the development version via anonymous CVS(Concurrent Version System):see the Developer Manual(Doc/developer man.pdf),section”Using CVS”.The Quantum ESPRESSO distribution contains several directories.Some of them are common to all packages:Modules/sourcefiles for modules that are common to all programsinclude/files*.h included by fortran and C sourcefilesclib/external libraries written in Cflib/external libraries written in Fortraniotk/Input/Output Toolkitinstall/installation scripts and utilitiespseudo/pseudopotentialfiles used by examplesupftools/converters to unified pseudopotential format(UPF)examples/sample input and outputfilesDoc/general documentationwhile others are specific to a single package:PW/PWscf:sourcefiles for scf calculations(pw.x)pwtools/PWscf:sourcefiles for miscellaneous analysis programstests/PWscf:automated testsPP/PostProc:sourcefiles for post-processing of pw.x datafilePH/PHonon:sourcefiles for phonon calculations(ph.x)and analysisGamma/PHonon:sourcefiles for Gamma-only phonon calculation(phcg.x)D3/PHonon:sourcefiles for third-order derivative calculations(d3.x)PWCOND/PWcond:sourcefiles for conductance calculations(pwcond.x)vdW/VdW:sourcefiles for molecular polarizability calculation atfinite frequency CPV/CP:sourcefiles for Car-Parrinello code(cp.x)atomic/atomic:sourcefiles for the pseudopotential generation package(ld1.x) atomic doc/Documentation,tests and examples for atomicGUI/PWGui:Graphical User Interface2.2PrerequisitesTo install Quantum ESPRESSO from source,you needfirst of all a minimal Unix envi-ronment:basically,a command shell(e.g.,bash or tcsh)and the utilities make,awk,sed. MS-Windows users need to have Cygwin(a UNIX environment which runs under Windows) installed:see /.Note that the scripts contained in the distribution assume that the local language is set to the standard,i.e.”C”;other settings may break them. Use export LC ALL=C(sh/bash)or setenv LC ALL C(csh/tcsh)to prevent any problem when running scripts(including installation scripts).Second,you need C and Fortran-95compilers.For parallel execution,you will also need MPI libraries and a“parallel”(i.e.MPI-aware)compiler.For massively parallel machines,or for simple multicore parallelization,an OpenMP-aware compiler and libraries are also required.Big machines with specialized hardware(e.g.IBM SP,CRAY,etc)typically have a Fortran-95compiler with MPI and OpenMP libraries bundled with the software.Workstations or“commodity”machines,using PC hardware,may or may not have the needed software.If not,you need either to buy a commercial product(e.g Portland)or to install an open-source compiler like gfortran or g95.Note that several commercial compilers are available free of charge under some license for academic or personal usage(e.g.Intel,Sun).2.3configureTo install the Quantum ESPRESSO source package,run the configure script.This is ac-tually a wrapper to the true configure,located in the install/subdirectory.configure will(try to)detect compilers and libraries available on your machine,and set up things accordingly. Presently it is expected to work on most Linux32-and64-bit PCs(all Intel and AMD CPUs)and PC clusters,SGI Altix,IBM SP machines,NEC SX,Cray XT machines,Mac OS X,MS-Windows PCs.It may work with some assistance also on other architectures(see below).Instructions for the impatient:cd espresso-X.Y.Z/./configuremake allSymlinks to executable programs will be placed in the bin/subdirectory.Note that both Cand Fortran compilers must be in your execution path,as specified in the PATH environment variable.Additional instructions for CRAY XT,NEC SX,Linux PowerPC machines with xlf:./configure ARCH=crayxt4./configure ARCH=necsx./configure ARCH=ppc64-mnconfigure Generates the followingfiles:install/make.sys compilation rules andflags(used by Makefile)install/configure.msg a report of the configuration run(not needed for compilation)install/config.log detailed log of the configuration run(may be needed for debugging) include/fft defs.h defines fortran variable for C pointer(used only by FFTW)include/c defs.h defines C to fortran calling conventionand a few more definitions used by CfilesNOTA BENE:unlike previous versions,configure no longer runs the makedeps.sh shell scriptthat updates dependencies.If you modify the sources,run./install/makedeps.sh or type make depend to updatefiles make.depend in the various subdirectories.You should always be able to compile the Quantum ESPRESSO suite of programs without having to edit any of the generatedfiles.However you may have to tune configure by specifying appropriate environment variables and/or command-line ually the tricky part is toget external libraries recognized and used:see Sec.2.4for details and hints.Environment variables may be set in any of these ways:export VARIABLE=value;./configure#sh,bash,kshsetenv VARIABLE value;./configure#csh,tcsh./configure VARIABLE=value#any shellSome environment variables that are relevant to configure are:ARCH label identifying the machine type(see below)F90,F77,CC names of Fortran95,Fortran77,and C compilersMPIF90name of parallel Fortran95compiler(using MPI)CPP sourcefile preprocessor(defaults to$CC-E)LD linker(defaults to$MPIF90)(C,F,F90,CPP,LD)FLAGS compilation/preprocessor/loaderflagsLIBDIRS extra directories where to search for librariesFor example,the following command line:./configure MPIF90=mpf90FFLAGS="-O2-assume byterecl"\CC=gcc CFLAGS=-O3LDFLAGS=-staticinstructs configure to use mpf90as Fortran95compiler withflags-O2-assume byterecl, gcc as C compiler withflags-O3,and to link withflag-static.Note that the value of FFLAGS must be quoted,because it contains spaces.NOTA BENE:do not pass compiler names with the leading path included.F90=f90xyz is ok,F90=/path/to/f90xyz is not.Do not use environmental variables with configure unless they are needed!try configure with no options as afirst step.If your machine type is unknown to configure,you may use the ARCH variable to suggest an architecture among supported ones.Some large parallel machines using a front-end(e.g. Cray XT)will actually need it,or else configure will correctly recognize the front-end but not the specialized compilation environment of those machines.In some cases,cross-compilation requires to specify the target machine with the--host option.This feature has not been extensively tested,but we had at least one successful report(compilation for NEC SX6on a PC).Currently supported architectures are:ia32Intel32-bit machines(x86)running Linuxia64Intel64-bit(Itanium)running Linuxx8664Intel and AMD64-bit running Linux-see note belowaix IBM AIX machinessolaris PC’s running SUN-Solarissparc Sun SPARC machinescrayxt4Cray XT4/5machinesmacppc Apple PowerPC machines running Mac OS Xmac686Apple Intel machines running Mac OS Xcygwin MS-Windows PCs with Cygwinnecsx NEC SX-6and SX-8machinesppc64Linux PowerPC machines,64bitsppc64-mn as above,with IBM xlf compilerNote:x8664replaces amd64since v.4.1.Cray Unicos machines,SGI machines with MIPS architecture,HP-Compaq Alphas are no longer supported since v.4.2.0.Finally,configure recognizes the following command-line options:--enable-parallel compile for parallel execution if possible(default:yes)--enable-openmp compile for openmp execution if possible(default:no)--enable-shared use shared libraries if available(default:yes)--disable-wrappers disable C to fortran wrapper check(default:enabled)--enable-signals enable signal trapping(default:disabled)and the following optional packages:--with-internal-blas compile with internal BLAS(default:no)--with-internal-lapack compile with internal LAPACK(default:no)--with-scalapack use ScaLAPACK if available(default:yes)If you want to modify the configure script(advanced users only!),see the Developer Manual.2.3.1Manual configurationIf configure stops before the end,and you don’tfind a way tofix it,you have to write working make.sys,include/fft defs.h and include/c defs.hfiles.For the latter twofiles,follow the explanations in include/defs.h.README.If configure has run till the end,you should need only to edit make.sys.A few templates (each for a different machine type)are provided in the install/directory:they have names of the form Make.system,where system is a string identifying the architecture and compiler.The template used by configure is also found there as make.sys.in and contains explanations of the meaning of the various variables.The difficult part will be to locate libraries.Note that you will need to select appropriate preprocessingflags in conjunction with the desired or available libraries(e.g.you need to add-D FFTW)to DFLAGS if you want to link internal FFTW).For a correct choice of preprocessingflags,refer to the documentation in include/defs.h.README.NOTA BENE:If you change any settings(e.g.preprocessing,compilationflags)after a previous(successful or failed)compilation,you must run make clean before recompiling,unless you know exactly which routines are affected by the changed settings and how to force their recompilation.2.4LibrariesQuantum ESPRESSO makes use of the following external libraries:•BLAS(/blas/)and•LAPACK(/lapack/)for linear algebra•FFTW(/)for Fast Fourier TransformsA copy of the needed routines is provided with the distribution.However,when available, optimized vendor-specific libraries should be used:this often yields huge performance gains. BLAS and LAPACK Quantum ESPRESSO can use the following architecture-specific replacements for BLAS and LAPACK:MKL for Intel Linux PCsACML for AMD Linux PCsESSL for IBM machinesSCSL for SGI AltixSUNperf for SunIf none of these is available,we suggest that you use the optimized ATLAS library:see /.Note that ATLAS is not a complete replacement for LAPACK:it contains all of the BLAS,plus the LU code,plus the full storage Cholesky code. Follow the instructions in the ATLAS distributions to produce a full LAPACK replacement.Sergei Lisenkov reported success and good performances with optimized BLAS by Kazushige Goto.They can be freely downloaded,but not redistributed.See the”GotoBLAS2”item at /tacc-projects/.FFT Quantum ESPRESSO has an internal copy of an old FFTW version,and it can use the following vendor-specific FFT libraries:IBM ESSLSGI SCSLSUN sunperfNEC ASLAMD ACMLconfigure willfirst search for vendor-specific FFT libraries;if none is found,it will search for an external FFTW v.3library;if none is found,it will fall back to the internal copy of FFTW.If you have recent versions of MKL installed,you may try the FFTW interface provided with MKL.You will have to compile them(only sources are distributed with the MKL library) and to modifyfile make.sys accordingly(MKL must be linked after the FFTW-MKL interface)MPI libraries MPI libraries are usually needed for parallel execution(unless you are happy with OpenMP multicore parallelization).In well-configured machines,configure shouldfind the appropriate parallel compiler for you,and this shouldfind the appropriate libraries.Since often this doesn’t happen,especially on PC clusters,see Sec.2.7.5.Other libraries Quantum ESPRESSO can use the MASS vector math library from IBM, if available(only on AIX).2.4.1If optimized libraries are not foundThe configure script attempts tofind optimized libraries,but may fail if they have been in-stalled in non-standard places.You should examine thefinal value of BLAS LIBS,LAPACK LIBS, FFT LIBS,MPI LIBS(if needed),MASS LIBS(IBM only),either in the output of configure or in the generated make.sys,to check whether it found all the libraries that you intend to use.If some library was not found,you can specify a list of directories to search in the envi-ronment variable LIBDIRS,and rerun configure;directories in the list must be separated by spaces.For example:./configure LIBDIRS="/opt/intel/mkl70/lib/32/usr/lib/math"If this still fails,you may set some or all of the*LIBS variables manually and retry.For example:./configure BLAS_LIBS="-L/usr/lib/math-lf77blas-latlas_sse"Beware that in this case,configure will blindly accept the specified value,and won’t do any extra search.。
电气英语试题及答案
电气英语试题及答案一、选择题(每题2分,共20分)1. Which of the following is not a type of electrical conductor?A. Copper wireB. GlassC. AluminumD. Graphite答案:B2. The unit of electric current is:A. VoltB. AmpereC. OhmD. Watt答案:B3. What is the term used to describe the flow of electric charge?A. VoltageB. CurrentC. ResistanceD. Power答案:B4. In an electrical circuit, what is the term for the total amount of electrical energy used?A. VoltageB. CurrentC. PowerD. Energy答案:D5. What is the basic unit of electrical resistance?A. OhmB. VoltC. AmpereD. Coulomb答案:A6. Which of the following is not a type of electrical energy source?A. Solar panelsB. Wind turbinesC. BatteriesD. Water heaters答案:D7. What is the term for the rate at which electric power is transferred by an electrical circuit?A. VoltageB. CurrentC. PowerD. Resistance答案:C8. The process of converting electrical energy into another form of energy is called:A. ConductionB. ConversionC. GenerationD. Transmission答案:B9. What is the term used to describe the potential difference between two points in an electrical circuit?A. CurrentB. VoltageC. PowerD. Resistance答案:B10. Which of the following is not a type of electricalcircuit component?A. ResistorB. CapacitorC. InductorD. Transformer答案:D二、填空题(每题2分,共20分)1. The electrical device that converts electrical energy into mechanical energy is called a ________.答案:motor2. The unit of electrical energy is the ________.答案:kilowatt-hour3. The electrical device that stores electrical energy is called a ________.答案:capacitor4. The electrical device that changes the voltage level in an electrical circuit is called a ________.答案:transformer5. The electrical device that protects the circuit from excessive current is called a ________.答案:fuse6. The process of converting mechanical energy intoelectrical energy is called ________.答案:generation7. The electrical device that allows current to flow in only one direction is called a ________.答案:diode8. The electrical device that changes alternating current (AC) to direct current (DC) is called a ________.答案:rectifier9. The electrical device that resists the flow of electric current is called a ________.答案:resistor10. The electrical device that stores electrical energy in a magnetic field is called an ________.答案:inductor三、简答题(每题10分,共30分)1. Explain the difference between voltage and current in an electrical circuit.答案:Voltage is the potential difference between two points in an electrical circuit, measured in volts (V). It is the force that pushes electric charge through a conductor. Current, on the other hand, is the flow of electric charge, measured in amperes (A). It is the rate at which electric charge passes a given point in the circuit.2. What is the function of a circuit breaker in an electrical system?答案:A circuit breaker is a safety device designed toprotect an electrical circuit from damage caused by excess current. It automatically cuts off the flow of electricity when the current exceeds a safe level, preventing potential hazards such as electrical fires or damage to appliances.3. Describe the role of a generator in an electrical power system.答案:A generator is a device that converts mechanical energy into electrical energy. In an electrical power system,generators are used to produce electricity by converting the kinetic energy from rotating turbines into electrical energy. This electricity is then transmitted and distributed to consumers through a network of power lines.。
2011年最新(英文)南洋理工大学NTU能源安全战略(Energy Security)教程21共24
5
MEASURING ENERGY SECURITY IMPLICATIONS OF FOSSIL FUEL RESOURCE CONCENTRATION
A need for alternative assessment tools
„Expert judgment‟ is not sufficient to assist government to decide if action is necessary to reduce energy insecurity, and if yes, what action to take. Climate change issue is also recognised as another driver of energy policy Key for policy makers to establish effective energy policy that achieves multiple goals, i.e. price-risk, supply-risk and climate change mitigations New tools are put forth to help policy makers assess energy insecurity
Energy security price index (ESPI) The measure of market concentration in competitive fossil fuel markets, Energy security physical availability index (ESPAI) The measure of supply flexibility in regulated markets.
energy environmental science文章模板 -回复
energy environmental science文章模板-回复Energy environmental science is a field that focuses on studying the impact of energy production and consumption on the environment. It aims to find sustainable and clean sources of energy to reduce the harmful effects on our planet. In this article, we will discuss the importance of energy environmental science and the steps to achieve a more sustainable future.1. Introduction to Energy Environmental ScienceEnergy is an essential component of our daily lives as it powers our homes, transportation, and industries. However, the traditional sources of energy, such as fossil fuels, have adverse effects on our environment. These effects include air and water pollution, climate change, and biodiversity loss. To mitigate these environmental impacts, energy environmental science plays a pivotal role in finding solutions for a sustainable energy future.2. The Importance of Energy Environmental ScienceEnergy environmental science is crucial for several reasons. Firstly, it helps us understand the negative impacts of traditional energy sources and the urgency to shift towards cleaner alternatives. This knowledge aids policymakers in formulating effective energy and environmental policies. Secondly, energy environmental science offers innovative technologies andmeasures to reduce energy consumption and promote renewable energy sources. Lastly, it raises awareness among the general public about the need for sustainable energy solutions, leading to changes in behavior and lifestyle patterns.3. Steps towards a Sustainable Energy Futurea. Promoting Renewable Energy SourcesRenewable energy sources, such as solar, wind, and hydroelectric power, provide a clean and sustainable alternative to fossil fuels. The first step towards a sustainable energy future is to increase the investment and deployment of renewable energy technologies. Governments should provide incentives and subsidies to encourage the use of renewable energy in residential, commercial, and industrial sectors. Additionally, research and development in renewable energy technologies should be intensified to enhance efficiency and cost-effectiveness.b. Energy Efficiency and ConservationEnergy efficiency and conservation are essential in reducing energy consumption and minimizing waste. This can be achieved by implementing energy-efficient technologies and practices in buildings, transportation, and manufacturing industries. Government regulations should be put in place to enforce energy-saving standards, such as building codes and vehicleemission standards. Moreover, public awareness campaigns can educate individuals on how small actions like turning off lights and appliances when not in use can make a significant impact.c. Carbon Capture and Storage (CCS)Despite efforts to shift towards renewable energy, some sectors still heavily rely on fossil fuels. Carbon capture and storage (CCS) technology can help mitigate the environmental impact of these industries. It captures carbon dioxide emissions from power plants and industrial facilities and stores them underground, preventing them from entering the atmosphere. Governments and industries should invest in research and development of CCS technology to make it more efficient and cost-effective.d. Transition to Sustainable TransportThe transportation sector is a significant contributor to greenhouse gas emissions. To achieve a sustainable energy future, we must promote the adoption of electric vehicles (EVs) and improve public transportation systems. Governments can provide incentives for purchasing EVs and expand charging infrastructure. Additionally, developing more efficient public transportation networks can reduce the overall energy consumption and emissions from transportation.e. International Collaboration and Policy FrameworksAchieving a sustainable energy future requires international collaboration and the establishment of policy frameworks. Countries should collaborate on research and development, share best practices, and work together to address global energy and environmental challenges. International agreements, such as the Paris Agreement, provide a framework for countries to set targets and commit to reducing greenhouse gas emissions.4. ConclusionEnergy environmental science plays a crucial role in addressing the environmental challenges associated with energy production and consumption. By promoting renewable energy sources, energy efficiency, carbon capture and storage, sustainable transport, and international collaboration, we can work towards a sustainable energy future. The transition to cleaner and more sustainable energy systems is not only essential for protecting the environment but also for ensuring the well-being and prosperity of future generations.。
对于能源的讨论英文作文
对于能源的讨论英文作文下载温馨提示:该文档是我店铺精心编制而成,希望大家下载以后,能够帮助大家解决实际的问题。
文档下载后可定制随意修改,请根据实际需要进行相应的调整和使用,谢谢!并且,本店铺为大家提供各种各样类型的实用资料,如教育随笔、日记赏析、句子摘抄、古诗大全、经典美文、话题作文、工作总结、词语解析、文案摘录、其他资料等等,如想了解不同资料格式和写法,敬请关注!Download tips: This document is carefully compiled by theeditor. I hope that after you download them,they can help yousolve practical problems. The document can be customized andmodified after downloading,please adjust and use it according toactual needs, thank you!In addition, our shop provides you with various types ofpractical materials,such as educational essays, diaryappreciation,sentence excerpts,ancient poems,classic articles,topic composition,work summary,word parsing,copyexcerpts,other materials and so on,want to know different data formats andwriting methods,please pay attention!Energy is really important in our daily lives. We use it for everything, from powering our homes to fueling our cars. Without energy, life would be very different.Some people think that renewable energy sources like solar and wind are the future. They're clean and don't cause as much pollution as fossil fuels. But they can be unreliable sometimes.Then there's nuclear energy. It can produce a lot of power, but there are concerns about safety and waste disposal.We also need to think about how we use energy. We should all try to be more energy-efficient to save money and help the environment. Like turning off lights when we leave a room or using energy-saving appliances.And what about the future of energy? Will we find newsources or better ways to use the ones we have? That's something to think about.。
Energy Neutral Wastewater Treatment
Energy Neutral Wastewater Treatment Wastewater treatment is a crucial process that ensures that water is safe for human consumption and the environment. However, the process of treating wastewater consumes a significant amount of energy, which contributes to the depletion of non-renewable resources and increases greenhouse gas emissions. Therefore, the need for energy-neutral wastewater treatment has become a critical issue in the water industry. In this essay, wewill explore the concept of energy-neutral wastewater treatment, its benefits, and challenges.Energy-neutral wastewater treatment refers to a process that generates as much energy as it consumes or even produces excess energy. The process involves the use of innovative technologies such as anaerobic digestion, biogas production, and energy recovery systems. These technologies enable the treatment plant to generate energy from the wastewater itself, reducing the reliance on external energy sources. The energy generated can be used to power the treatment plant or even supply electricity back to the grid.The benefits of energy-neutral wastewater treatment are numerous. Firstly, it reduces the carbon footprint of the treatment plant, contributing to the mitigation of climate change. Secondly, it reduces the operational costs of the treatment plant, as it relies less on external energy sources. Thirdly, it promotes sustainability by utilizing renewable resources and reducing the dependency on non-renewable resources. Lastly, it enhances the resilience of the treatment plant by ensuring a consistent and reliable energy supply.However, energy-neutral wastewater treatment comes with its challenges. Firstly, the implementation of innovative technologies requires significant capital investment, which may not be feasible for smaller treatment plants. Secondly, the maintenance and operation of these technologies require specialized skills and knowledge, which may not be readily available. Thirdly, the variability of the wastewater composition and flow rate may affect the efficiency of the energy recovery systems. Lastly, the production of biogas may require additional treatment to remove impurities, which may add to the operational costs.To overcome these challenges, it is essential to develop a comprehensive strategy that includes technology selection, financial planning, and capacity building. The strategy should prioritize the implementation of technologies that are suitable for the specific wastewater composition and flow rate. Additionally, it should explore alternative financing mechanisms such as public-private partnerships, grants, and loans. Moreover, it should provide training and capacity building programs for the staff to ensure the proper operation and maintenance of the energy recovery systems.In conclusion, energy-neutral wastewater treatment is a viable solution to address the energy consumption and environmental impact of wastewater treatment. It offers numerous benefits such as reducing the carbon footprint, promoting sustainability, and enhancing the resilience of the treatment plant. However, it comes with its challenges, including capital investment, specialized skills and knowledge, variability of wastewater composition, and additional treatment requirements. To overcome these challenges, a comprehensive strategy that includes technology selection, financial planning, and capacity building is necessary. By implementing energy-neutral wastewater treatment, we can ensure a sustainable and resilient water future.。
- 1、下载文档前请自行甄别文档内容的完整性,平台不提供额外的编辑、内容补充、找答案等附加服务。
- 2、"仅部分预览"的文档,不可在线预览部分如存在完整性等问题,可反馈申请退款(可完整预览的文档不适用该条件!)。
- 3、如文档侵犯您的权益,请联系客服反馈,我们会尽快为您处理(人工客服工作时间:9:00-18:30)。
a rX iv:mat h /611221v1[mat h.ST]8Nov26The Annals of Statistics 2006,Vol.34,No.4,1636–1641DOI:10.1214/009053606000000470Main article DOI:10.1214/009053606000000515c Institute of Mathematical Statistics ,2006DISCUSSION OF “EQUI-ENERGY SAMPLER”BY KOU,ZHOU AND WONG By Peter Minary and Michael Levitt Stanford University Novel sampling algorithms can significantly impact open ques-tions in computational biology,most notably the in silico protein folding problem.By using computational methods,protein folding aims to find the three-dimensional structure of a protein chain given the sequence of its amino acid building blocks.The complexity of the problem strongly depends on the protein representation and its energy function.The more detailed the model,the more complex its corresponding energy function and the more challenge it sets for sampling algorithms.Kou,Zhou and Wong have introduced a novel sampling method,which could contribute significantly to the field of structural prediction.1.Rough 1D energy landscape.Most of the energy functions describing off-lattice protein models are assembled from various contributions,some of which take account of the “soft”interactions between atoms (residues)far apart in sequence,while others represent the stiffconnections between atoms directly linked together with chemical bonds.As a consequence of this complex nature,the resulting energy function is unusually rough even for short protein chains.The authors apply the equi-energy (EE)sampler to a multimodal two-dimensional model distribution,which is an excellent test for sampling algo-rithms.However,it lacks the characteristic features of distributions derived from complex energy functions of off-lattice protein models.In studies con-ducted by Minary,Martyna and Tuckerman [1],the roughness of such energy surfaces was represented by using a Fourier series on the interval [0,L =10][see Figure 1(a)],h (x )=220i =1c (i )sin(i 2πx/L ),(1)2S.C.KOU,Q.ZHOU AND W.H.WONGFig.1.(a)The model system energy function,h(x)(dotted line),and the corresponding normalized distribution,f(x),scaled by a constant,c=200(solid line).(b)Comparing distributions produced by the EE sampler(EEMC)and parallel tempering(PT)to the tar-get distribution(black)after40,000iterations in the interval[0,8].(c)Similar comparison in the intervals[8,9.5]and[9.5,10].(d)Convergence rate∆f to the target distribution f(x)as a function of the number of iterations for the EE sampler with energy disk sizes of5,000(solid black),10,000(dashed black)and2,500(dot-dashed black).The same quan-tity is plotted for parallel tempering(gray).The distributions presented in(b)and(c)are produced from statistics,collected up to40,000iterations(arrow).where the coefficients are(c1,c2,...,c20)=(0.21,1.25,0.61,0.25,0.13,0.10,1.16,0.18,0.12,0.23,0.21,0.19,0.37,0.99,0.36,0.02,0.06,0.08,0.09,0.04). The performance of various sampling algorithms on the energy function, h(x),is related to their ability to effectively locate the energy basins sep-arated by large energy barriers.In particular,previous studies by Minary, Martyna and Tuckerman[1]show that a superior convergence rate to the corresponding normalized distribution,1f(x)=DISCUSSION3Table1Sample size of energy ringsChain<−8.7[−8.7,−7.5)[−7.5,−5)[−5.0,−0.2)≥−0.2 to propagate the chains X(i),as it generates more efficient moves guided by the energy surface gradient.Furthermore,it is well suited to complex high-dimensional systems because it can produce collective moves.The initial values of the chains were obtained from a uniform distribution on[0,L] and the MD step size wasfinely tuned,so that the HMC acceptance ratio was in the range[0.4,0.5].Figure1shows that for all x∈[0,L],h(x)>−10,so that H0was set to−10.The energy levels,which were chosen by geometric progression in the interval[−10,10],are reported together with the temperature levels in Table1.The EE jump probability p ee was set to0.15and each chain was equilibrated for an initial period prior to the production sampling of100,000iterations.The sizes of the energy rings were bounded,as computer memory is limited,especially when applying the EE sampler to structure prediction problems.After their sizes reach the upper bound,the energy rings are refreshed by replacing randomly chosen elements.In Table1,the number of samples present in each energy ring after the initial burn-in period is summarized.It shows that energy rings corresponding to lower-order chains are rich in low-energy elements,whereas higher-order chains are rich in high-energy elements.For benchmarking the performance of the EE sampler,parallel tempering (PT)trajectories of the same length were generated using the same number of HMC chains,temperature levels and exchange probabilities.The aver-age acceptance ratio for EE jumps and replica exchange in PT was0.82 and0.45,respectively.Figures1(b)and(c)compare the analytical distribu-tions,f(x),with the numerical ones produced by the EE sampler and PT after40,000iterations.All the minima of f(x)are visited by both methods within this fraction of the whole sampling trajectory.Quantitative compari-son is obtained via the average distance between the produced and analytical distributions,1∆f(f k,f)=4S.C.KOU,Q.ZHOU AND W.H.WONGwhere f k is the instantaneously computed numerical distribution at the k th iteration and N is the number of bins used.Figure1(d)depicts∆f,as a function of the number of MC iterations.It is clear that a substantial gain in efficiency is obtained with the EE sampler,although the convergence rate is dependent on the maximum size of energy disks.2.Off-lattice protein folding in three dimensions.Efficient sampling and optimization over a complex energy function are regarded as the most severe barrier to ab initio protein structure prediction.Here,we test the perfor-mance of the EE sampler in locating the native-like conformation of a sim-plified united-residue off-latticeβ-sheet protein introduced by Sorenson and Head-Gordon[4]based on the early works of Honeycutt and Thirumalai[3]. The model consists of46pseudoatoms representing residues of three differ-ent types:hydrophobic(B),hydrophilic(L)and neutral(N).The potential energy contains bonding,bending,torsional and intermolecular interactions:h=46i=2k bond2(θi−θ0)2 +46i=4[A(1+cosφ)+B(1+cos3φ)](4)+46i=1,j≥+3V XY(r ij),X,Y=B,L or N.Here,k bond=1000εH˚A−2,σ=1˚A,k bend=20εH rad−2,θ0=105◦;εH= 1000K(Kelvin);the torsional potentials have two types:if the dihedral an-gles involve two or more neutral residues,A=0,B=0.2εH(flexible angles), and otherwise A=B=1.2εH(rigid angles).The nonbonded interactions are bead-pair specific,and are given by V BB=4εH[(σ/r ij)12−(σ/r ij)6], V LX=8/3εH[(σ/r ij)12+(σ/r ij)6]for X=B or L and V NX=4ε[(σ/r ij)12] with X=B,L or N.This model and its energy function are illustrated in Figure2.A particular sequence of“amino acids,”(BL)2B5N3(LB)4N3B9N3(LB)5L, is known to fold into aβ-barrel conformation as its global minimum energy structure with the potential energy function given above.Thus,this system is an excellent test of various sampling algorithms such as the EE sampler or parallel tempering.Since the native structure is known to be the global minimum(h min)on the energy surface,H0was set to h min−0.05|h min|.The energy corresponding to the completely unfolded state(h unf)serves as an approximate upper bound to the energy function because all the favorable nonbonded interactions are eliminated.This is true only if we assume that bond lengths and bend angles are kept close to their ideal values and thereDISCUSSION5paring equi-energy Monte Carlo(EEMC)and parallel tempering(PT)to fold3D off-latticeβ-sheet model proteins with known native structure.Thefigure shows the united-residue model with three types of residues:hydrophobic(black),hydrophilic(gray) and neutral(light gray).The energy function contains contributions from bonds,bends, torsions and intermolecular interactions,the last being attractive between hydrophobic–hy-drophobic residues and repulsive otherwise.The circular image in the center of thefigure illustrates some of the ten initial structures,which were generated by randomizing the tor-sions in the loop regions.These torsions are defined as the ones which include more than two neutral residues.The three“RMSD from native vs.MC steps”subplots contain repre-sentative trajectories starting from the three encircled configurations,whose distance from the native state(s n)was∼3.0,6.0and9.0˚A,respectively.The last subplot gives the probability that a visited structure is contained in the set S x={s:RMSD(s,s n)≤x˚A}, PT(gray)and EEMC(black).are no“high-energy collisions”between nonbonded beads.K was taken to be8so that nine HMC chains were employed.First,the energy levels H1,...,H8were chosen to follow a geometric progression in[H0,H8+1=h unf],but this produced an average EE jump acceptance ratio of0.5.In order to increase the acceptance,the condi-tion for geometric progression was relaxed.The following alternative was used:(a)create an energy ladder by using H i+1=H iλ;(b)uniformly scale H1,...,H8+1so that H8+1=h unf.Applying this strategy and using aλ6S.C.KOU,Q.ZHOU AND W.H.WONGdrawn from[1.1,1.2]produced an average EE jump acceptance ratio of∼0.8. The equi-energy probability p ee was set to0.15and the parameters for the HMC chains X(i)were chosen in the same way as discussed in the case of the1D model problem.To test the ability of EEMC and PT to locate the native structure,ten initial structures were obtained by randomly altering the loop region torsion angles.Then both EEMC and PT trajectories starting from the same initial configurations were generated.For each structure(s)the RMSD deviation from the native state(s n)was monitored as a function of the number of MC iterations.The three representative trajectories depicted in Figure2 start from initial structures with increasing RMSD distance from the native structure.Some trajectories demonstrate the superior performance of the EE sampler over PT,since the native state is found with fewer MC iterations. More quantitative comparison is provided by the probability distribution of the RMSD distance,P(x),which was based on a statistic collected from all the ten trajectories.As Figure2indicates,the cumulative integral of the distribution shows that50%of the structures visited by the EE sampler are in S1.5where S x={s:RMSD(s,s n)≤x˚A}.The corresponding number for PT is25%.These tests show that the EE sampler can offer sampling efficiency bet-ter than that of other state-of-the-art sampling methods such as parallel tempering.Careful considerations must be made when choosing the setting for the energy levels and disk sizes for a given number of chains.Further-more,we believe that proper utilization of the structural information stored in each energy disk could lead to the development of novel,more powerful topology-based optimization methods.REFERENCES[1]Minary,P.,Martyna,G.J.and Tuckerman,M.E.(2003).Algorithms and novelapplications based on the isokinetic ensemble.I.Biophysical and path integralmolecular dynamics.J.Chemical Physics1182510–2526.[2]Duane,S.,Kennedy,A.D.,Pendleton,B.J.and Roweth,D.(1987).HybridMonte Carlo.Phys.Lett.B195216–222.[3]Honeycutt,J.D.and Thirumalai,D.(1990).Metastability of the folded statesof globular A873526–3529.[4]Sorenson,J.M.and Head-Gordon,T.(1999).Redesigning the hydrophobic coreof a modelβ-sheet protein:Destabilizing traps through a threading approach.Proteins:Structure,Function and Genetics37582–591.Department of Structural BiologyStanford UniversityStanford,California94305USAE-mail:peter.minary@michael.levitt@。