The electromagnetic effects in isospin symmetry breakings of q{bar q} systems

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Effect of external magnetic field on electron spin dephasing induced by hyperfine interacti

Effect of external magnetic field on electron spin dephasing induced by hyperfine interacti
(February 1, 2008)
Abstract
We investigate the influence of an external magnetic field on spin phase relaxation of single electrons in semiconductor quantum dots induced by the hyperfine interaction. The basic decay mechanism is attributed to the dispersion of local effective nuclear fields over the ensemble of quantum dots. The characteristics of electron spin dephasing is analyzed by taking an average over the nuclear spin distribution. We find that the dephasing rate can be estimated as a spin precession frequency caused primarily by the mean value of the local nuclear magnetic field. Furthermore, it is shown that the hyperfine interaction does not fully depolarize electron spin. The loss of initial spin polarization during the dephasing process depends strongly on the external magnetic field, leading to the possibility of effective suppression of this mechanism.

Gamma2

Gamma2

u ? d djN i = gA U (p) U (p) ; (1) where U (p) denotes the nucleon spinor. Assuming isospin symmetry, one nds (gA )p = ?(gA )n, and the value of (gA)p = 1:2573 0:0028, extracted from the neutron beta decay, has been quoted in the literature 1]. In nature, the isospin symmetryis broken by the current quark mass di erence as well as the electromagnetic interaction, and thus (gA )p 6= ?(gA )n . Previous studies of the nucleon isovector axial charge in the framework of external eld QCD sum-rule method have been made by various authors 2{4]. However, to our best knowledge, the isospin breaking e ects have been ignored in these studies. The goal of this Letter is to examine the di erence between (gA )p and (gA)n using the external eld QCD sum-rule approach, which has been used in studying various nucleon matrix elements of bilinear quark operators 2{13]. The isospin violation is re ected in mu 6= md and the isospin breaking in the vacuum condensates. Electromagnetic e ects will not be included. Invoking the Goldberger-Treiman relation, we also give an estimate of the isospin breaking in the pion-nucleon coupling constants, which is of interest in the investigation of charge symmetry breaking phenomena 14{17]. Let us start from the correlation function of the nucleon interpolating eld in the presence of a constant external isovector axial vector eld Z

MIL-STD-1275E

MIL-STD-1275E

METRICMIL-STD-1275E22 MARCH 2013SUPERSEDINGMIL-STD-1275D29 August 2006 DEPARTMENT OF DEFENSEINTERFACE STANDARDCHARACTERISTICS OF28 VOLT DC INPUT POWER TO UTILIZATION EQUIPMENT INMILITARY VEHICLESFOREWORD1.This standard is approved for use by all departments and agencies of the Department of Defense (DOD).2.The intent of this document is to describe the nominal 28 VDC voltage characteristics, common across military ground vehicles, at the input power terminal of the utilizing electrical and electronic assemblies directly connected to the distribution network. This lays the groundwork for commonality across vehicle pla tforms. The vehicle’s design authority is responsible to ensure that the 28 VDC delivered to the input power terminal of the utilization equipment meets these requirements.3.This is neither a power source nor a power system standard. This standard focuses on utilization equipment and the conditions under which it is expected to operate.ments, suggestions, or questions on this document should be addressed to U.S. Army Tank automotive and Armaments Command, ATTN: RDTA-EN/STND/TRANS, MS# 268, 6501 E. 11 Mile Road, Warren, MI 48397 5000 or emailed to usarmy.detroit.rdecom.mbx.tardec-standardization@. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at https://.Table of Contents1 SCOPE (1)1.1 Scope. (1)2 APPLICABLE DOCUMENTS (1)2.1 General. (1)2.2 Government documents (1)2.2.1 Specifications, standards, and handbooks. (1)2.3 Non-Government documents. (1)2.4 Order of precedence. (2)3 DEFINITIONS (2)3.1 Utilization equipment. (2)3.2 Equipment under test. (2)3.3 Operations. (2)3.3.1 Starting operation. (2)3.3.2 Normal operation. (2)3.4 Operational voltage range. (2)3.5 Transient waveform characteristics. (2)3.5.1 Rise time. (2)3.5.2 Fall time. (3)3.5.3 Recovery time. (3)3.5.4 Ripple. (3)3.6 Types of transient waveforms. (3)3.6.1 Starting disturbance. (3)3.6.2 Voltage spike. (4)3.6.3 Voltage surge. (5)3.6.4 Intermittent contact. (6)3.7 Reverse polarity (6)4 GENERAL REQUIREMENTS (6)4.1 Reverse polarity (6)4.2 Electromagnetic compatibility. (7)4.3 Electrostatic discharge (7)5 DETAILED REQUIREMENTS (7)5.1 Voltage compatibility requirements. (7)5.1.1 Steady state operation. (7)5.1.2 Starting operation. (7)5.1.3 Transient disturbances. (8)5.2 Voltage compatibility verification setup. (9)5.2.1 Environmental conditions. (9)5.2.2 Calibration of test equipment. (10)5.2.3 Nominal voltage. (10)5.2.4 Measurement tolerance. (10)5.2.5 Measurement reference point. (11)5.2.6 Power return. (11)5.2.7 Loads. (11)5.2.8 Power supply. (11)5.3 Voltage compatibility verification method. (11)5.3.1 Steady state operation. (11)5.3.2 Starting operation. (12)5.3.3 Transient disturbances. (12)5.3.4 Reverse polarity. (15)5.3.5 Electromagnetic compatibility. (15)5.3.6 Electrostatic discharge. (15)6 NOTES (15)6.1 Intended use (15)6.2 Acronyms. (15)6.3 International interest. (16)6.4 Changes from previous issue (16)6.5 Subject term (key word) listing. (16)Table of FiguresFigure 1. Recovery time. (3)Figure 2. Sample starting disturbance waveform. (4)Figure 3. Voltage spike. (4)Figure 4. Sample alternator load dump waveform. (5)Figure 5. Sample intermittent contact waveform. (6)Figure 6. Starting disturbance limits on 28VDC systems. (8)Figure 7. Envelope of spikes for 28VDC systems. (9)Figure 8. Envelope of surges for 28VDC systems. (10)Figure 9. Sample test setup for immunity to injected voltage spikes. (12)Figure 10. Sample test setup for exported voltage spikes and surges. (13)Figure 11. Sample test circuit for immunity to injected voltage surges. (14)Table of TablesTable I. Positive voltage surge test parameters. (14)1SCOPE1.1Scope.This standard defines the operating voltage limits and transient voltage characteristics of the 28 VDC electrical power at the input power terminals to the utilization equipment connected to the electrical power distribution system on military ground vehicle platforms.2APPLICABLE DOCUMENTS2.1General.The documents listed in this section are cited in sections 3, 4 and 5 of this document. This section does not include documents cited in other sections of this standard or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, the users of this standard are cautioned that they must meet all requirements of documents cited in sections 3, 4 and 5 of this standard, whether or not they are listed in this section.2.2Government documents.2.2.1Specifications, standards, and handbooks.The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract.DEPARTMENT OF DEFENSEMIL-STD-461 - Requirements for the Control of ElectromagneticInterference Characteristics of Subsystems and Equipment(Copies of these documents are available from https:///quicksearch/ or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.)2.3Non-Government documents.The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of documents are those cited in the solicitation or contract.SAE INTERNATIONALSAE J1113-42 - Electromagnetic Compatibility—Component TestProcedure—Part 42—Conducted Transient Emissions(Copies of these documents are available from or SAE Customer Service, 400 Commonwealth Drive, Warrendale, PA 15096-0001.)2.4Order of precedence.In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption is obtained in writing from the applicable authority.3DEFINITIONS3.1Utilization equipment.Utilization equipment is defined as the electronic device, equipment, or system subjected to the voltage range(s) indicated in this specification.3.2Equipment under test.The Equipment Under Test (EUT) is defined as the electronic device, equipment, or system undergoing validation and/or verification testing or evaluation.3.3Operations.3.3.1Starting operation.Electrical power during an engine starting event is sufficient for utilization equipment to provide the level of performance specified in the utilization equipment’s detailed specification.3.3.2Normal operation.Electrical power is sufficient for utilization equipment to provide the level of performance specified in the utilization equipment’s detailed specification.3.4Operational voltage range.Voltage characteristics representative of the nominal operating voltage within a pre-defined tolerance or limit. Some variation in voltage is reasonable and expected; however, this variation remains within pre-defined limits of operation.3.5Transient waveform characteristics.A transient waveform represents a time-varying electrical signal defined by characteristics such as rise/fall time, period, frequency of oscillation, pulse width, etc. Transients typically exceed pre-defined steady-state limits, return to and remain within the steady-state limits within a specified time. The transient may have positive or negative polarity and/or be of short or long duration. Transient voltage levels may also exceed the system battery voltage by several hundred volts depending on the source of the transient.3.5.1Rise time.The rise time is the difference between when the rising edge of a voltage or current transient crosses a pre-defined low threshold to when the transient crosses a pre-defined high threshold. As defined in this standard, the low threshold is defined to be the time at when the amplitude of the rising edge is equal to ten percent (10%) of the maximum value of the transient. The highthreshold is defined to be the time when the amplitude is equal to ninety percent (90%) of the maximum value of the transient.3.5.2Fall time.The fall time is the difference between when the falling edge of a voltage or current transient crosses a pre-defined high threshold to when the transient crosses a pre-defined low threshold. As defined in this standard, the high threshold is defined to be the time at when the amplitude of the falling edge is equal to ninety percent (90%) of the maximum value of the transient. The low threshold is defined to be the time when the amplitude is equal to ten percent (10%) of the maximum value of the transient.3.5.3Recovery time.The interval between the time a characteristic deviates from the steady-state limits and the time it returns and remains within the same range. Refer to Figure 1.Figure 1. Recovery time.3.5.4Ripple.The regular and/or irregular variations of voltage about a fixed DC voltage level during normal operation of a DC system.3.6Types of transient waveforms.There are several different types of transient waveforms associated with the vehicle’s power supply system.3.6.1Starting disturbance.A starting disturbance is the variation in system voltage from the normal operating voltage range caused by the initial engagement of the engine starter and subsequent engine cranking. The duration of the Initial Engagement Surge (IES) is measured from the time at which it departs from the normal operating voltage to the time at which it reaches and remains at the crankingvoltage. An example showing “Initial Engagement Surge” (IES) and “Cranking”; i.e., voltage level during active engine cranking is shown in Figure 2.Figure 2. Sample starting disturbance waveform.3.6.2 Voltage spike.A voltage spike is an energy-limited transient waveform having a duration less than or equal to 1 ms. These typically result from the interaction of the power delivery system wiring and switching of reactive loads or a mismatch in impedance between the wiring harness andequipment. Figure 3 shows an example of a spike waveform.Figure 3. Voltage spike.V peak t duration Timef osc0.1 V peak0.9 V peak0 VDC t rise3.6.3 Voltage surge.A surge is a transient waveform having a duration greater than 1 ms and a specific wave shape, typically a rising/falling edge and a slow exponential decay for the falling edge. Surges result from the switching of reactive loads containing a significant level of stored energy or sudden disconnection of a constant load. Surges may also occur due to the application of high-demand loads.3.6.3.1 Positive voltage surge.A positive voltage surge is a positive-going transient, which exceeds the nominal supplied voltage. This may occur when a high current or inductive load is suddenly disconnected. The most common occurrence of a positive voltage surge, or “alternator load dump,” occurs when the alternator is working to charge a partially or fully discharged set of batteries and the connection to the battery positive terminal is suddenly disconnected. The alternator cannot immediately decrease its output to compensate for the sudden loss of load so the energy delivered during this settling period is distributed to the vehicle’s electrical system. A positive surge (V PEAK ) with a short rise time (t RISE ) and long exponential decay is generated above the nominal battery voltage of the system (V NOM ) and last for a given time (t WIDTH ). Figure 4 shows an example of an alternator load dump waveform.Figure 4. Sample alternator load dump waveform.3.6.3.2 Negative voltage surge.This event is similar to an alternator load dump as specified in Section 3.6.3.1 except itrepresents the negative-going transient generated when a sudden load is placed on the alternator. The alternator cannot immediately change its output so the system voltage decreases until the alternator can compensate for the sudden increase in load.VoltV V3.6.4 Intermittent contact.Intermittent contact occurs when electrical contacts in a switch or relay change state. A common way of describing intermittent contacts is the use of t he terms “contact bounce” or “chattering relay.” Mechanical vibration may also affect the operation of mechanical contacts and cause this to occur. The settling period and pulse widths associated may vary depending on theconstruction of the contacts. Figure 5 shows an example of an intermittent contact waveform.Figure 5. Sample intermittent contact waveform.Intermittent contact may affect operation of equipment in one of two ways. First, equipment power feed(s) controlled by the relay/switch may be directly affected with resets, dropouts, etc. Second, the electrical noise generated by the intermittent contact on a directly connected wire may be coupled to nearby wires in the wiring harness through electric/magnetic field coupling.3.7 Reverse polarity.Reverse polarity is d efined as the inverted connection of the EUT’s power terminal(s) to the vehicle’s power system. The positive (+) terminal of the EUT is connected to the negative (-) or “ground” terminal of the vehicle’s power supply system. The negative (-) terminal of the EUT is connected to the positive (+) terminal of the vehicle’s power supply system.4 GENERAL REQUIREMENTS4.1 Reverse polarity.Utilization equipment shall protect itself against damage due to input power with reverse polarity. With reverse polarity voltage applied to the input power terminals of the utilization equipment, the magnitude of the reverse polarity input current shall be equal to or less than the magnitude of the utilization equipment normal operating current.VoltV4.2 Electromagnetic compatibility.Utilization equipment shall be compatible with the applicable performance specificationrequirements for control of electromagnetic interference and voltage spikes induced by lightning, electromagnetic pulses, and power switching. Electromagnetic interference is not covered by this standard.4.3 Electrostatic discharge.Utilization equipment shall be compatible with the applicable performance specificationrequirements for immunity to electrostatic discharge. Electrostatic discharge is not covered by this standard. 5 DETAILED REQUIREMENTS5.1 Voltage compatibility requirements.This section contains detailed requirements regarding the voltage conditions under which the utilization equipment is expected to operate. Verification of compliance shall be in accordance with Sections 5.2 and 5.3 of this document.5.1.1disturbances, and applies to all utilization equipment. Utilization equipment shall operatewithout degradation or damage when subjected to the operational voltage range specified in this section.5.1.1.1 Operational voltage range.The utilization equipment voltage operating range is between 20 VDC and 33 VDC, including ripple.5.1.1.2 Voltage ripple.The maximum peak-to-peak ripple voltage limits are specified in MIL-STD-461 CS101 with the same values used at 150 kHz extended to 250 kHz, as shown in Figure CS101-1.5.1.2 disturbances. Utilization equipment shall operate without degradation or damage when subjected to engine starting disturbances within the limits shown in Figure6.5.1.2.1 Initial engagement surge (IES).The minimum voltage supplied to utilization equipment during an IES is 12 VDC. Themaximum duration of the IES is one (1) second. Consecutive IES events are a minimum of one (1) second apart.5.1.2.2 Cranking surges.The minimum voltage supplied to utilization equipment during cranking surges is 16 VDC. The maximum duration of cranking surges is thirty (30) seconds.Figure 6. Starting disturbance limits on 28VDC systems.5.1.3Transient disturbances.5.1.3.1 Voltage spikes.5.1.3.1.1 Injected voltage spikes.Utilization equipment shall operate without degradation or damage when subjected to voltage spikes within the limits shown in Figure 7. The maximum rise time (t RISE ) of the injected spikes is 50 nanoseconds, and the maximum total energy content of a single spike is 2 Joules.5.1.3.1.2 Emitted voltage spikes.Emitted voltage spikes from utilization equipment shall be within the limits shown in Figure 7. The maximum total energy content of a single emitted spike is 125 millijoules (mJ).5.1.3.2 Voltage surges.5.1.3.2.1 Injected voltage surges.Utilization equipment shall operate without degradation or damage when subjected to voltage surges within the limits shown in Figure 8. The maximum total energy content of a single surge is 60 Joules (J).Time (s)Figure 7. Envelope of spikes for 28VDC systems.5.1.3.2.2 Emitted voltage surges.Emitted voltage surges from utilization equipment shall be within the limits shown in Figure 8.5.2 Voltage compatibility verification setup.5.2.1 Environmental conditions.Testing of the EUT according to this standard shall be performed under the following environmental conditions:Temperature: +23°C ± 5°C (+73°F ± 9°F) Relative Humidity: 0% to 90% humidity Atmospheric Pressure: 80kPa to 102kPa (23.62 inHg to 30.12 inHg)Testing under different environmental conditions (e.g., extremes of operating temperature) shall be conducted at the discretion of the appropriate authority.The electromagnetic environment (e.g., background noise) shall not interfere with the measurement instrumentation setup.1002003004005006007008009001000Time (µs)Volts1 100 200 300 400 500 600 700 800 900 1000Time (ms)Figure 8. Envelope of surges for 28VDC systems.5.2.2Calibration of test equipment.Test equipment used to verify parameters such as current, voltage, rise/fall time, etc. of the test setup shall have traceable calibration to a national standards body, such as NIST, and within the calibration period at the time of the test.5.2.3Nominal voltage.For purposes of verification, the term “nominal” when used to describe voltage shall mean the stated voltage ±1%, unless otherwise stated.5.2.4Measurement tolerance.The default measurement tolerance shall be ±1% unless otherwise stated.5.2.5Measurement reference point.The measurement reference point for EUTs shall be the power input terminals of the EUT. EUTs having multiple power input terminals shall be individually and simultaneously monitored during the test(s). All transient voltage waveforms applied to EUTs shall be verified open circuit; i.e., no load.5.2.6Power return.The test setup shall use a power return for the EUT as required by the applicable performance specification.If a power return is not specified, the EUT power return conductor shall be equivalent to the EUT power source conductor.In cases where the EUT uses the vehicle structure as the power return, a ground plane in accordance with (IAW) MIL-STD-461 shall be used to simulate the vehicle’s metal structure as the return current path. The negative (-) terminal of the EUT as well as the negative (-) terminal of the power source shall be bonded to the ground plane.5.2.7Loads.Loads representative of the actual installation on vehicle shall be used to test the EUT if the EUT is not a standalone device.5.2.8Power supply.Power supplies shall maintain ±1% of specified voltage during testing, as measured at their output.5.3Voltage compatibility verification method.5.3.1Steady state operation.5.3.1.1Operational voltage range.The EUT shall be tested to operate as specified while subjected to the voltages/durations at both the lower and higher limits of the voltage envelope shown in Figure 8. Any deviation from normal operation shall be recognized as a failure of the EUT.5.3.1.2Voltage ripple.Unless otherwise specified in the applicable performance specification, the test method and limits for voltage ripple specified in MIL-STD-461 CS101 shall be used at nominal voltages of 23 VDC and 30 VDC with the same values used at 150 kHz extended to 250 kHz, as shown in Figures CS101-1 and CS101-2.Verify the EUT operates as specified while subjected to the ripple. Any deviation from normal operation shall be recognized as a failure of the EUT.5.3.2Starting operation.When applicable, the EUT shall be tested to operate as specified while subjected to the voltages/durations of the lower limit of the voltage envelope shown in Figure 6. Any deviation from normal operation shall be recognized as a failure of the EUT.5.3.3Transient disturbances.5.3.3.1Voltage spikes.5.3.3.1.1Injected voltage spikes.The EUT shall be supplied power by a voltage source set to the nominal 28 VDC operating voltage through a Line Impedance Stabilization Network (LISN). The test operator shall inject voltage spikes into the EUT using a test setup similar to Figure 9.Figure 9. Sample test setup for immunity to injected voltage spikes.One LISN shall be used when the power return is the vehicle chassis; in this case the ground plane provides the power return current path. Two LISNs shall be used when the EUT has a dedicated power return conductor, such as wires, buss bar, etc. This simulates the additional vehicle wiring harness present in the vehicle.Both positive and negative voltage spikes shall be applied to the EUT. A minimum of fifty (50) 250V spikes of each polarity shall be applied at one (1) second intervals. Each test spike shall have a peak amplitude of 250V, a risetime not exceeding 50 ns, a frequency of oscillation greater than 100 kHz and less than 500 kHz, and a maximum energy content of 2 Joules.Verify the EUT operates as specified while subjected to the voltage spikes. Any deviation from normal operation shall be recognized as a failure of the EUT.5.3.3.1.2Emitted spikes.The EUT shall be supplied power by a source set to the nominal 28 VDC operating voltage. Unless otherwise specified in the applicable performance specification, use the conducted transient emissions test method specified in SAE J1113-42 to measure the spikes emitted by the EUT using a test setup similar to Figure .Figure 10. Sample test setup for exported voltage spikes and surges.One LISN shall be used when the power return is the vehicle chassis; in this case the ground plane provides the power return current path. Two LISNs shall be used when the EUT has a dedicated power return conductor, such as wires, buss bar, etc. This simulates the additional vehicle wiring harness present in the vehicle.The test operator shall exercise switching function(s) of the EUT capable of producing spikes, (e.g., the switching of any inductive loads controlled by the EUT). If the power source to the EUT is controlled by means of a vehicle mounted switch or relay, the test shall be performed using this switch or relay. Each switching function shall be exercised a minimum of thirty-two (32) times in order to give a reasonable probability that the maximum spike voltage is recorded. The test operator shall monitor the operation of the EUT. Voltage spikes emitted by the EUT shall be within the limits shown in Figure 7. Any voltage spike or combination of voltage spikes emitted from a single event shall have an energy content less than 125 mJ.5.3.3.2Voltage surges.5.3.3.2.1Injected voltage surges.The test operator shall inject voltage surges into the EUT using a test setup similar to Figure 11.Figure 11. Sample test circuit for immunity to injected voltage surges.The voltage waveform injected on the power line(s) of the EUT shall simulate the voltage surge shown in Figure 4. The voltage surge parameters are shown in Table I. Energy emitted from the transient surge generator shall be limited to 60 Joules.Prior to connection of the EUT, the test operator shall verify the amplitude and duration of the voltage surge specified in Table I with a non-inductive load whose resistance is matched to the source impedance of the transient generator.Verify the EUT operates as specified while subjected to the voltage surges. Any deviation from normal operation shall be recognized as a failure of the EUT.5.3.3.2.2Emitted voltage surges.The EUT shall be supplied power by a source set to the nominal 28 VDC operating voltage. The test operator shall measure voltage surges emitted by the EUT using a test setup similar to Figure 10. The test operator shall exercise function(s) of the EUT capable of producing surges. Each surge-producing function shall be exercised a minimum of thirty-two (32) times in order to give a reasonable probability that the maximum surge voltage is recorded.The test operator shall monitor the operation of the EUT. Voltage surges emitted by the EUT shall be within the limits shown in Figure 8.5.3.4Reverse polarity.Connect the positive (+) terminal of the EUT to the negative (-) terminal of the power supply system. Connect the negative (-) terminal of the EUT to the positive (+) terminal of the power supply system. Set the voltage on the power supply to 33 VDC and leave connected for five (5) minutes. Connect EUT input terminals to power with the correct polarity and verify device operates as specified. Any deviation from normal operation shall be recognized as a failure of the EUT.5.3.5Electromagnetic compatibility.The EUT shall demonstrate compliance with the applicable performance specification requirements for control of electromagnetic interference and voltage spikes induced by lightning, electromagnetic pulses, and power switching prior to MIL-STD-1275 testing. Electromagnetic interference testing is not covered by this standard.5.3.6Electrostatic discharge.The EUT shall demonstrate compliance with the applicable performance specification requirements for immunity to electrostatic discharge prior to MIL-STD-1275 testing. Electrostatic discharge testing is not covered by this standard.6NOTES(This section contains information of a general or explanatory nature, which may be helpful, but is not mandatory.)6.1Intended use.The intent of this document is to describe the nominal 28 VDC voltage characteristics, common across military ground vehicles, at the input power terminal of the utilizing electrical and electronic assemblies directly connected to the distribution network. This lays the groundwork for commonality across vehicle platforms. The vehicle’s design authority is responsible to ensure that the 28 VDC delivered to the input power terminal of the utilization equipment meets these requirements.6.2Acronyms.6.3International interest.Certain provisions of this standard are the subject of international standardization agreement NATO STANAG 2601. When a change notice, revision, or cancellation of this standard is proposed which will modify the international agreement concerned, the preparing activity will take appropriate action through international standardization channels, including departmental standardization offices, to change the agreement or make other appropriate accommodations. 6.4Changes from previous issue.Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes.6.5Subject term (key word) listing.PolarityRecovery timeRippleRise timeSpikeStarting disturbanceSurgeVoltageCustodian: Preparing Activity: Army – AT Army - ATReview Activities: Project 2920-2013-001 Army - CR, MI, TEDLA - CCNOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online, database at https://.。

ELECTROMAGNETIC

ELECTROMAGNETIC

Some of the advantages of eddy current inspection include:
• • • • • • • • Sensitive to small cracks and other defects Detects surface and near surface defects Inspection gives immediate results Equipment is very portable Method can be used for much more than flaw detection Minimum part preparation is required Test probe does not need to contact the part Inspects complex shapes and sizes of conductive materials

The maximum value of eddy current located on the surface. The eddy current is reduced inside the object control
TYPES OF CONTROLLED DEFECTS
• • • • • Discontinuities; Cracks; The bundles (violation of structure); Sinks; Non-metallic inclusions.
The method is non-contact.
Test result does not depend on the humidity, pressure, dust, radioactive radiation, contamination of non-conductive surface layer.

经典电磁学英文教程

经典电磁学英文教程

经典电磁学英文教程A classic electromagnetic theory English course is a comprehensive study of the fundamental principles and concepts of electromagnetism. This course covers topics such as electromagnetic fields, electromagnetic waves, Maxwell's equations, and electromagnetic properties of materials.The course begins with an introduction to the basic laws and principles of electromagnetism, including Coulomb's law, Gauss's law, and Ampere's law. Students learn about electric and magnetic fields and how they are related through Maxwell's equations.The course then delves into the properties of electromagnetic waves, including their propagation, polarization, and interference. Students learn about the different types of electromagnetic waves, such as radio waves, microwaves, and light waves.In addition to theoretical concepts, the course also covers practical applications of electromagnetism. Students learn about the behavior of electromagnetic waves in different media and their interaction with matter. They also learn about the applications of electromagnetism in areas such as telecommunications, electronics, and optics.Throughout the course, students are exposed to various mathematical techniques and problem-solving strategies to analyze and solve electromagnetic problems. This includes vector calculus, differential equations, and Fourier analysis.Overall, a classic electromagnetic theory English course provides students with a deep understanding of the principles and applications of electromagnetism. It lays the foundation for further studies in fields such as electrical engineering, physics, and telecommunications.。

激发三重态(Excitedthreestates)

激发三重态(Excitedthreestates)

激发三重态(Excited three states)At most temperatures, most molecules are at the lowest vibrational level of the ground state. Molecules absorbed in the ground state absorb energy (electric energy, thermal energy, chemical energy, or light energy, etc.) and are excited to be excited. The excited state is very unstable,It will release energy quickly and re jump back to the ground state. When the molecules return to the ground state, the energy is emitted in the form of emission of electromagnetic radiation (light), known as luminescence". If the molecules of matter absorb light energy, they are stimulatedThe electromagnetic radiation emitted by the transition back to the ground state, known as fluorescence and phosphorescence. The mechanism of fluorescence and phosphorescence is discussed in terms of molecular structure theory.Each molecule has a series of strictly separated energy levels, called electron energy poles, and each electron energy level contains a series of vibrational energy levels and rotational energy levels. The state of motion of electrons in moleculesIn addition to the energy levels, the electrons contain multiple states of electrons. In M=2S+1, S is the sum of the quantum numbers of each electron spin quantum, with a value of 0 or 1. According to the principle of Pauli incompatibility, the same orbital in the moleculeThe two electrons occupied must have opposite spin directions, namely spin pairing. If all electrons in the molecule are spinpaired, then S=0, M=1, the molecule is in a singlet state (or a single line), expressed in symbolic S.The ground states of most organic compounds are in the singlet state. When the ground state molecules absorb energy, if the electron does not change in the direction of spin during the transition, it is still M=1, and the molecules are excited at a single weightIf the electron is accompanied by a change in the spin direction during the transition, then the molecule has two spin unpaired electrons, S=1, M=3, and the molecule is in the excited three state, expressed in symbolic T.Fig. 14.1 is a schematic diagram of electronic states.Fig. 14.1 sketch of excitation of three heavy states in a singlet stateThe unpaired electrons in discrete orbits are more stable than spin pairs (especially the rules), so in the same excited state, the energy levels of the three states are always slightly lower than those of the singlet state.Fig. 14.2 is a diagram of energy levels and transitions, in which S0, S1 and S2 represent the ground states of the molecules, the first and second electron excited singlet states, respectively, and T1 and T2 represent the three and second electron excited states of the molecule respectively. V=0, 1, 2, 3,... Represents the vibrational level of theground state and excited state.Fig. 14.2 energy level diagram of fluorescence and phosphorescence systemThe molecules in the excited state are very unstable, which may be activated by means of radiative transitions and nonradiative transitions (de excitation), releasing excess energy and returning to the ground state.Radiation transitions are mainly related to fluorescence, delayed fluorescence or phosphorescence emission; nonradiative transition is the release of excess energy in the form of heat, including vibrational relaxation, internal transfer, intersystem crossing and external transferCheng. Fig. 14.2 represents the energy transfer process of molecular excitation and deactivation:(1) vibrational relaxation (Vibration, relaxation, abbreviated as VR) - the transition from the lowest vibrational energy level (V=0) of the ground state to the excited singlet state may be possible when the molecules absorb the radiation of light (as shown in lambda 1, lambda 2 in Fig. 14.2)Higher vibrational levels of Sn (as shown in S1 and S2). Then,In the gas phase where the liquid phase or the pressure is high enough, the collision probability between molecules is large, and the molecules may pass excess vibrational energy to the surrounding region in the form of heatEnvironment, and its transition from the high vibrational energy level of the excited state to the lowest vibrational level of the electron energy level, this process is called vibrational relaxation. The vibrational relaxation time is 10 - 12s orders of magnitude.(2) internal transfer (Internal, conversion, abbreviated as IC) - when the low vibrational energy levels in the high electron levels overlap with the high vibrational energy levels in the lower electron levels, electrons frequently occur from the high electron energy levelsThe transition from nonradiative to low electron levels. As shown in Fig. 14. and 2, the low vibrational kinetic energy levels in S2 and T2 overlap with the high vibrational kinetic energy levels in S1 and T1, and electrons can transition from S2 to S1 through the superposition of vibrational levels, or fromT2 transition to T1. This process is called internal transfer. Time transfer for 1011s ~ 1013s magnitude. The rate of vibrational relaxation and internal transfer is much faster than the direct emission of photons by a highly excited state,Therefore, no matter which excited singlet state excited by the radiation energy, the molecules can jump to the lowest vibrational level via vibrational relaxation and internal transfer to the lowest (first) excited singlet state.(3) fluorescence emission (Fluorescence, emission, FE) - afterthe vibrational relaxation and internal transfer of electrons in the excited singlet state, reach the lowest vibrational level (V=0) of the first excited singlet (S1),The vibrational levels of the ground state (S0) transition in the form of radiation. The process is fluorescence emission with a fluorescence wavelength of. The energy loss due to vibrational relaxation and internal transfer, and hence the fluorescence emission energyThe energy is smaller than the molecular absorption, and the wavelength of fluorescence emission is longer than the wavelength of molecular absorption. The average lifetime of the lowest vibrational level in the first excited singlet state is about 10-9 - 10 - 4S, so the fluorescence lifetime is also in the rangeThis order of magnitude.(4) department (Intersystem Crossing, ISC Kuayue) - between leap refers to the non radiative transition process between different multiplets, it relates to the electronic excited spin state change.Such as the transition from the first excited singlet state S1 to the first excited three heavy state T1, so that the two spin pairs of electrons are no longer paired. This transition is prohibited (not in conformity with the spectral selection rule),But if the two energy layers have a large overlap, the minimumvibrational level of S1 in Figure 14.2 overlaps with the higher vibrational levels of T1, and it is possible to achieve this transition by spin orbit coupling.Between leap slower and experience a long time.(5) (Phosphorescence emission, PE luminescence emission) - the electronic excited state by the Department after three leap reach the excited state, after the rapid relaxation of vibrational relaxation and the transition to the first excited state threeThe lowest vibrational energy levels are then converted in the form of radiation back to the vibrational levels of the ground state, which are emitted by phosphorescence. The transition of the phosphorescence emission is still the spin forbidden, so the light speed is very slow.The life of 10-4 ~ 100s phosphor. Therefore, after the external light source is stopped, phosphorescence remains a short time. After the system vibration leap and T1 lost a part of the energy relaxation,So the phosphorescence wavelength is longer than the fluorescence wavelength, that is, the wavelength is longer than the wavelength of the phosphor.It must be pointed out that T1 may also be re excited by thermal excitation back to S1, i.e., T1S1, and then converted back to S0 by radiation from S1, S1S0, which emits fluorescence, which is called delayed fluorescence,Its lifetime is similar to that of phosphorescence, but its wavelength is shorter than phosphorescence.(6) external transfer (External, convertion, EC) - excited state molecules collide with solvent molecules or other solute molecules, and the process of energy transfer is called external transfer.External transfer can weaken or even weaken the intensity of fluorescence or phosphorescence. This phenomenon is called quenching or quenching.。

The Nature of Electromagnetic Radiation

The Nature of Electromagnetic Radiation

The Nature of ElectromagneticRadiationElectromagnetic radiation is a fundamental aspect of the universe that surrounds us. It is an essential component of our daily lives, from the light we see to the radio waves that allow us to communicate with one another. In this article, we will delve into the nature of electromagnetic radiation and explore its various properties.Electromagnetic radiation, as the name suggests, is made up of two components: electric and magnetic fields. These fields are perpendicular to each other and propagate through space as waves. Electromagnetic waves are transverse waves, which means that the direction of their vibration is perpendicular to the direction of their propagation. In contrast, longitudinal waves vibrate in the same direction as their propagation.The electromagnetic spectrum is a continuum of electromagnetic waves that range from low frequency, low energy radio waves to high frequency, high energy X-rays and gamma rays. The spectrum is divided into several regions, each of which corresponds to a different range of frequencies and wavelengths. The most familiar region of the spectrum is the visible region, which corresponds to the light that we can see with our eyes.The behavior of electromagnetic waves is governed by several fundamental principles. One of the most important of these is the inverse square law, which states that the intensity of the radiation decreases with distance from the source in proportion to the square of the distance. This means that if we move twice as far away from a source of radiation, the intensity of the radiation will decrease by a factor of four.Another fundamental principle is the law of reflection, which states that when a wave strikes a surface, it is reflected back at an angle equal to the angle of incidence. This principle is what allows us to see ourselves in a mirror, as well as to use radar to measure the distance to an object.Electromagnetic waves also exhibit properties such as diffraction and interference. Diffraction occurs when a wave encounters an obstruction, causing it to spread out and bend around the edges of the obstruction. Interference occurs when two waves meet and combine, resulting in either reinforcement or cancellation of the waves.The behavior of electromagnetic radiation is also affected by the medium through which it passes. For example, light travels at different speeds in different materials, a property known as refractive index. This is why a straw appears to bend when it is placed in a glass of water.One of the most surprising properties of electromagnetic radiation is its wave-particle duality. This means that electromagnetic radiation exhibits both wave and particle-like behavior, depending on how it is observed. This property is what allows us to build electronic devices, such as computers and smartphones, that rely on the behavior of individual particles of radiation.In conclusion, electromagnetic radiation is a fundamental aspect of the universe that surrounds us. It is a complex and fascinating phenomenon that plays a vital role in our daily lives. Understanding the nature of electromagnetic radiation is essential for many modern technologies, from cell phones to space telescopes.。

电科专业英语复习资料

电科专业英语复习资料

电科专业英语复习资料T ext1_Exercise? 1.the microprocessor is the central①component(部件)of the PC.? 2.Reliability and Stability:The quality of the processor is one factor thatdetermines②how reliably your system will run(系统运行的可靠性).While most processors are very③dependable (可靠的),some are not.This also depends④to some extent(在某种程度上)on the age of processor and how much energy it⑤consumes(消耗).? 3.Flash memory is a①solid state(固态的)storage device-everything is②electronic(电子的).Flash memory provides a③non-volatile(非易失的),reliable,low power,low cost,④high density(高密度)storage device for programmable⑤code and data(代码和数据),making it extremely useful in the⑥embedded(嵌入式)marketplace.翻译:? 1.芯片是嵌入了集成电路的一小片半导体材料。

? 1.A chip is a small piece of semiconducting materialon which an integrated circuitis embedded.?2.典型芯片不足1平方英寸,却能包含几百万个晶体管。

电磁操控 英语

电磁操控 英语

电磁操控英语Electromagnetic Manipulation。

Introduction。

Electromagnetic manipulation refers to the control and manipulation of objects using electromagnetic forces. This technology has found various applications in different fields, including robotics, medicine, and industry. In this document, we will explore the principles behind electromagnetic manipulation and its wide range of applications.Principles of Electromagnetic Manipulation。

Electromagnetic manipulation is based on the fundamental principles of electromagnetism. It involves the interaction between electric currents and magnetic fields. According to the right-hand rule, when an electric current flows through a conductor, a magnetic field is generated around it. By manipulating the strength and direction of this magnetic field, we can control the movement and behavior of objects.Electromagnets and Magnetic Fields。

热激发自旋电子学(SpinCalortronics)

热激发自旋电子学(SpinCalortronics)

熱激發自旋電子學(Spin Caloritronics)本所李尚凡副研究員、美國約翰霍浦金斯大學天文與物理系錢嘉陵教授、與台大凝態中心郭瑞年主任部分由國科會龍門計畫支持組成的跨國研究團隊,在新興研究領域“熱激發自旋電子學”(Spin Caloritronics)獲得突破性的重大研究成果。

藉由建立溫度差來控制熱流、電荷與自旋電流目前主流的研究方式是希望藉由平行膜面的溫度差,驅動自旋電流,當自旋向上與自旋向下電子數不相等時,自旋極化電流便因應而生。

然而室溫下藉由熱激發所產生的自旋電動勢與外加磁場呈非對稱關係。

目前尚無法解釋為何在遠大於自旋擴散長度,且物理性質完全不同的材料中,得到類似的結果。

我們的研究團隊首次以實驗證實,藉由熱激發的非對稱自旋電動勢也可經由垂直膜面的溫度差來驅動,系統化地翻轉熱自旋電動勢。

在沒有基板的磁性箔片可確保只有水平方向的溫度梯度存在,實驗發現熱電動勢為對稱的行為。

此重要發現有助了解熱激發自旋電子學的機制與過程,並為相關研究領域提供一個全新的思考方向。

本研究成果論文將發表於標竿期刊《物理評論通訊》(Physical Review Letters, 107, 216604 (2011))。

A team lead by Dr. Shang-Fan Lee, Prof. C. L. Chien of Department of Physics and Astronomy in the Johns Hopkins University, and Prof. J. Raynein Kwo in CCMS of NTU, also supported by the Dragon Gate Program under the NSC, has important results on the newly developed ‘Spin Caloritronics’. Most studies of spin caloritronic effects to date, including spin-Seebeck effect, utilize thin films on substrates. We use patterned ferromagnetic thin film to demonstrate the profound effect of a substrate on the spin-dependent thermal transport. With different sample patterns and on varying the direction of temperature gradient, both longitudinal and transverse thermal voltages exhibit asymmetric instead of symmetric spin dependence. This unexpected behavior is due to an out-of-plane temperature gradient imposed by the thermal conduction through the substrate and the mixture of anomalous Nernst effects. Only with substrate-free samples have we determined the intrinsic spin-dependent thermal transport with characteristics and field sensitivity similar to those of the anisotropic magnetoresistance effect. The result has been published in Physical Review Letters, 107, 216604 (2011).圖一、(a)鎳鐵奈米線與熱電動勢的量測示意圖;(b)不同角度下熱電動勢對外加磁場的關係;(c)由左至右與(d)由右至左的平行膜面溫度差下,熱電動勢與角度的關係。

感应加热工作原理中英文对照

感应加热工作原理中英文对照

感应加热工作原理中英文对照induction Heating operating principle感应加热应用了两条物理定律。

楞次定律和焦耳效应。

任何导电材料放在可变磁场(由一个名为感应器的励磁绕组产生)中,产生感应电流,即为涡流。

根据焦耳定律(P =R x I²),电流在其所在金属中散热。

为了最大限度的产生能量,金属需要被快速加热。

Induction heating results from the direct application of two physical laws, the LENZ law and the JOULE effect:any electrically conductive material placed in a variable magnetic field (generated by an exciting winding called inductor) is the site of induced electric currents, called eddy currents. Due to the Joule effect (P =R x I²), these currents dissipate heat in the material in which they appeared.In order to transfer a maximum amount of energy to the part to be treated, The heat generated in the material implies a quick response and a high efficiency.感应加热需要考虑的因素Several parameters must be taken into consideration:●感应器各自的位置和特征。

The Science of Electromagnetic Compatibility

The Science of Electromagnetic Compatibility

The Science of ElectromagneticCompatibility电磁兼容性科学作为一个现代人,我们周围无处不在电磁波,从智能手机到计算机、电视、微波炉、射频识别器等等。

但是,当设备之间的电磁场相互干扰时,就会产生问题,这就是电磁兼容性问题。

本文将讨论电磁兼容性科学。

什么是电磁兼容性?电磁兼容性是指在电磁环境中不同设备之间可能发生的两个问题:电磁干扰和电磁敏感性。

电磁干扰是指电子设备中的信号受到其他设备辐射的电磁干扰。

这种干扰可能会导致系统的错误或中断。

电磁敏感性是指电子设备受到其他设备辐射的电磁场的影响,导致系统性能下降或失效。

因此,为了确保设备之间的互操作性,避免电磁兼容性问题,必须对电磁场的传播和电子设备的辐射进行评估和测试。

这就需要使用电磁兼容性科学。

电磁兼容性科学电磁兼容性科学是研究电磁干扰和电磁敏感性的科学。

它不仅涉及电磁场的传播和辐射特性,还包括设备和系统的电磁特性、结构和复杂的电路设计等方面。

电磁兼容性科学可以分为三个主要领域:电磁场的理论、电磁场的实验和电磁场测试。

其中,电磁场的理论可以分为数学模型和计算机仿真。

数学模型是基于电磁场方程,通过数学公式和方法,计算电磁场在不同条件下的传播和辐射特性。

计算机仿真则是通过建立计算机模型来模拟电磁场的传播和辐射特性。

这些方法可以帮助设计人员预测电磁场的特性,以及在设计和测试电子设备时确保电磁兼容性。

电磁场的实验是指使用实验设备和测量方法,对电子设备辐射和电磁干扰进行评估和测试。

这涉及到电磁场测试设备的设计和构造、测试方法和测量结果的数据分析和解释。

电磁场的实验是评估和测试电磁兼容性的重要手段。

电磁场测试是指在实际情况下对电磁场进行测试的方法。

这种测试包括开发特定场景的电磁场实验室或测试设备以及对设备和系统在不同工作环境下进行测试。

这涉及到电磁场测试结果的数据处理和分析。

总之,电磁兼容性科学提供了评估电子设备兼容性的方法,以确保电子设备在电磁环境中的正常工作。

On the particle acceleration near the light surface of radio pulsars

On the particle acceleration near the light surface of radio pulsars

a r X i v :a s t r o -p h /0002525v 1 29 F eb 2000Mon.Not.R.Astron.Soc.000,1–??(1999)Printed 1February 2008(MN L A T E X style file v1.4)On the particle acceleration near the light surface of radiopulsarsV.S.Beskin 1,2and R.R.Rafikov 31National Astronomical Observatory,Osawa 2–21–1,Mitaka,Tokyo 181–8588,Japan 2P.N.Lebedev Physical Institute,Leninsky prosp.,53,Moscow,117924,Russia 3Princeton University Observatory,Princeton,NJ,08544,USAAccepted 1999.Received 1999;in original form 1999ABSTRACTThe two–fluid effects on the radial outflow of relativistic electron–positron plasma are considered.It is shown that for large enough Michel (1969)magnetization param-eter σ≫1and multiplication parameter λ=n/n GJ ≫1one–fluid MHD approxima-tion remains correct in the whole region |E |<|B |.In the case when the longitudinal electric current is smaller than the Goldreich–Julian one,the acceleration of particles near the light surface |E |=|B |is determined.It is shown that,as in the previously considered (Beskin Gurevich &Istomin 1983)cylindrical geometry,almost all electro-magnetic energy is transformed into the energy of particles in the narrow boundary layer ∆̟/̟∼λ−1.Key words:two–fluid relativistic MHD:radio pulsars—particle acceleration1INTRODUCTIONDespite the fact that the structure of the magnetosphere of radio pulsars remains one of the fundamental astrophysical problems,the common view on the key theoretical question –what is the physical nature of the neutron star braking –is absent (Michel 1991,Beskin Gurevich &Istomin 1993,Mestel 1999).Nevertheless,very extensive theoretical studies in the seventies and the eighties allowed to obtain some model-independent results.One of them is the absence of magnetodipole energy loss.This result was first obtained theoretically (Henriksen &Norton 1975,Beskin et al 1983).It was shown that the electric charges filling the magnetosphere screen fully the magnetodipole radiation of a neutron star for an arbitrary inclination angle χbetween the rotational and magnetic axes if there are no longitudinal currents flowing in the ter this result was also confirmed by observations.The direct detections of the interaction of the pulsar wind with a companion star in close binaries (see e.g.Djorgovsky &Evans 1988,Kulkarni &Hester 1988)have shown that it is impossible to explain the heating of the companion by a low–frequency magnetodipole wave.On the other hand,the detailed mechanism of particle acceleration remains unclear.Indeed,a very high magnetization parameter σ(Michel 1969)in the pulsar magnetosphere demonstrates that within the light cylinder r <R L =c/Ωthe main part of the energy is transported by the Poynting flux.It means that the additional mechanism of particle acceleration must work in the vicinity of the light cylinder.It is necessary to stress that an effective particle acceleration can only take place for small enough longitudinal electric currents I <I GJ when the plasma has no possibility to pass smoothly through the fast magnetosonic surface and when the light surface |E |=|B |is located at a finite distance.As to the case of the large longitudinal currents I >I GJ ,both analytical (Tomimatsu 1994,Begelman &Li 1994,Beskin et al 1998)and numerical (Bogovalov 1997)considerations demonstrate that the acceleration becomes ineffective outside the fast magnetosonic surface,and the particle-to-Poynting flux ratio remains small:∼σ−2/3(Michel 1969,Okamoto 1978).The acceleration of an electron–positron plasma near the light surface was considered by Beskin Gurevich and Istomin (1983)in the simple 1D cylindrical geometry for I ≪I GJ .It was shown that in a narrow boundary layer ∆̟/̟∼1/λalmost all electromagnetic energy is actually converted to the particles energy.Nevertheless,cylindrical geometry does not provide the complete picture of particle acceleration.In particular,it was impossible to include self–consistently the disturbance of a poloidal magnetic field and an electric potential,the later playing the main role in the problem of the plasma acceleration (for more details see e.g.Mestel &Shibata 1994).Hence,a more careful 2D consideration is necessary.c1999RAS2V.S.Beskin and R.R.RafikovIn Sect.2we formulate a complete system of2D two–fluid MHD equations describing the electron–positron outflow from a magnetized body with a monopole magneticfield.The presence of an exact analytical force–free solution(Michel 1973)allows us to linearize this system which results in the existence of invariants(energy and angular momentum)along unperturbed monopolefield lines similar to the ideal one–fluid MHDflow.In Sect.3it is shown that forσ≫1andλ≫1 (λ=n/n GJ is the multiplication factor)the one–fluid MHD approximation remains true in the entire region within the light surface.Finally,in Sect.4the acceleration of particles near the light surface|E|=|B|is considered.It is shown that,as in the case of cylindrical geometry,in a narrow boundary layer∆̟/̟∼λ−1almost all the electromagnetic energy is converted into the energy of particles.2BASIC EQUATIONSLet us consider a stationary axisymmetric outflow of a two–component plasma in the vicinity of an active object with a monopole magneticfield.It is necessary to stress that,of course,the monopole magneticfield is a rather crude approximation for a pulsar magnetosphere.Nevertheless,even for a dipole magneticfield near the origin,at large distances r≫R L in the wind zone the magneticfield can have a monopole–like structure.For this reason the disturbance of a monopole magnetic field can give us an important information concerning particle acceleration far from the neutron star.The structure of theflow is described by the set of Maxwell‘s equations and the equations of motion∇E=4πρe,∇×E=0,∇B=0,∇×B=4πc×B.(2)Here E and B are the electric and magneticfields,ρe and j are the charge and current densities,and v±and p±are the speed and momentum of particles.In the limit of infinite particle energyγ=∞,v0r=c,v0ϕ=0,v0θ=0,(3) and for charge and current densityρ0e=ρs R2sr2cosθ,(4)the monopole poloidal magneticfieldB0r=B sR2scR sccosθ,(7) and theflux functionΨ(r,θ),so thatB0p=∇Ψ×eϕ2πce R2s2cosθ+η+(r,θ) ,(9)n−=ΩB sr2 λ+1c[−cosθ+δ(r,θ)],(11)Ψ(r,θ)=2πB s R2s[1−cosθ+εf(r,θ)],(12)c 1999RAS,MNRAS000,1–??On the particle acceleration near the light surface of radio pulsars3v ±r=c1−ξ±r (r,θ),v ±θ=cξ±θ(r,θ),v ±ϕ=cξ±ϕ(r,θ),(13)B r =B sR 2ssin θ∂fr sin θ∂f cR s c ∂δcr−sin θ−∂δsin θ∂2cos θξ+r−λ+1∂rr2∂δsin θ∂∂θ=0,(20)∂ζrλ−12cos θξ−θ,(21)−ε∂r 2−ε∂θ 1∂θ=2Ω2cos θξ+ϕ−λ+1∂rξ+θγ++ξ+θγ+r ∂δr −sin θΩr2ξ+ϕ,(23)∂r=−4λσ −1∂θ+ζrξ−r +c∂rγ+=4λσ−∂δr ξ+θ,(25)∂∂r−sin θ∂rξ+ϕγ++ξ+ϕγ+Ωr sin θ∂fΩr 2ξ+θ,(27)∂r=−4λσ −εc∂r−c4λmc 3(29)is the Michel‘s (1969)magnetization parameter,m is the electron mass,and all deflecting functions are supposed to be ≪1.It is necessary to stress that for applications the magnetic field B s is to be taken near the light cylinder R s ≈R L because in the internal region of the pulsar magnetosphere B ∝r −3.As it has already been mentioned,only outside the light cylinder the poloidal magnetic field may have quasi monopole structure.As a result,σ=Ω2eB 0R 34V.S.Beskin and R.R.Rafikov1975,Arons Scharlemann 1979),γin ≤102for secondary plasma.For this reason in what follows we consider in more details the caseγ3in ≪σ,(34)when the additional acceleration of particles inside the fast magnetosonic surface takes place (see e.g.Beskin Kuznetsova Rafikov 1998).It is this case that can be realized for fast pulsars.Moreover,it has more general interest because the relation(34)may be true also for AGNs.As to the case γ3in ≫σcorresponding to ordinary pulsars,the particle energy remains constant (γ=γin )at any way up to the fast magnetosonic surface (see Bogovalov 1997for details).Further,one can putδ(R s ,θ)=0,(35)εf (R s ,θ)=0,(36)η+(R s ,θ)−η−(R s ,θ)=0.(37)These conditions result from the relation c E s +ΩR s e ϕ×B s =0corresponding rigid rotation and perfect conductivity of the surface of a star.Finally,as will be shown in Sect.3.2,the derivative ∂δ/∂r actually determines the phase of plasma oscillations only and plays no role in the global structure.Finally,the determination of the electric current and,say,the derivative ∂f/∂r depend on the problem under consideration.Indeed,as is well–known,the cold one–fluid MHD outflow contains two singular surfaces,Alfv´e nic and fast magnetosonic ones.It means that for the transonic flow two latter functions are to be determined from critical conditions (Heyvaerts 1996).In particular,the longitudinal electric current within this approach is not a free parameter.On the other hand,if the electric current is restricted by some physical reason,the flow cannot pass smoothly through the fast magnetosonic surface.In this case,which can be realized in the magnetosphere of radio pulsars (Beskin et al 1983,Beskin &Malyshkin 1998),near the light surface |E |=|B |an effective particle acceleration may take place.Such an acceleration will be considered in Sect.4.3THE ELECTRON–POSITRON OUTFLOW 3.1The MHD LimitIn the general case Eqns.(19)–(28)have several integrals.Firstly,Eqns.(21),(25),and (26)result in ζ−22σλsin θ=1sin θ,(38)where l (θ)describe the disturbance of the electric current at the star surface by the equation I (R,θ)=I A sin 2θ+l (θ).Expression (38)corresponds to conservation of the total energy flux along a magnetic field line.Furthermore,Eqns.(25)–(28)together with the boundary conditions (35),(36)result in δ=εf −1c ξ+ϕ+14λσγ−1−Ωr sin θ4λσγin .(40)They correspond to conservation of the z –component of the angular momentum for both types of particles.It is necessary to stress that the complete nonlinearized system of equations contains no such simple invariants.As σλ≫1,we can neglect in Eqns.(23)–(28)their left-hand sides.In this approximation we have ξ+=ξ−i.e.γ−=γ+=γ,so that −1∂θ+ζr ξr +c Ωr sin θ∂fΩr 2ξθ=0,(42)and γ1−Ωr sin θtan θεf +l (θ)σsin θ(γ−γin ).(45)c1999RAS,MNRAS 000,1–??On the particle acceleration near the light surface of radio pulsars5 Substituting these expressions into(41)and using Eqns.(19)–(22),we obtain the following equation describing the disturbance of the magnetic surfacesε(1−x2sin2θ)∂2fx2∂sinθ∂f∂x−2εsinθcosθ∂fsinθdσ(γ−γin)−sinθ∂θ−2λsin2θ(ξ+r−ξ−r)+2λxsinθ(ξ+ϕ−ξ−ϕ)≈0,(47)so actually there is perfect agreement with the MHD approximationε(1−x2sin2θ)∂2fx2∂sinθ∂f∂x−2εsinθcosθ∂fsinθdσ(γ−γin)−sinθ∂θ=0.As was shown earlier(Beskin et al1998),to pass through the fast magnetosonic surface it’s necessary to have|l|<σ−4/3.(49) Hence,within the fast magnetosonic surface r≪r F one can neglect terms containingδ=εf andζ.Then,relations(41)and (42)result inγ(1−x sinθξϕ)=γin,(50)ξr=ξϕ2ξr−ξ2ϕ,(53) we obtain forσ≫γ3in for r≪r Fγ2=γ2in+x2sin2θ,(54)ξϕ= x sinθ x sinθ,(55)ξr= x2sin2θ x2sin2θ,(56)in full agreement with the MHD results.Next,to determine the position of the fast magnetosonic surface r F,one can analyze the algebraic equations(38)and (41)which give−∂δtanθδ−1xξϕ=0.(57) Using now expressions(43)and(53),one canfind2γ3−2σ K+1∂θ.(59) Equation(58)allows us to determine the position of the fast magnetosonic surface and the energy of particles.Indeed, determining the derivative r∂γ/∂r,one can obtainr ∂γ3γ−σ(2K+x−2).(60)c 1999RAS,MNRAS000,1–??6V.S.Beskin and R.R.RafikovAs the fast magnetosonic surface is the X–point,both the nominator and denominator are to be equal to zero here.As a result,evaluating r∂K/∂r as K,we obtainδ∼σ−2/3;(61) r F∼σ1/3R L;(62)γ(r F)=σ1/3sin2/3θ,(63) where the last expression is exact.These equations coincide with those obtained within the MHD consideration.It is the self–consistent analysis whenδ=εf,and hence K depends on the radius r that results in thefinite value for the fast magnetosonic radius r F.On the other hand,in a given monopole magneticfield,whenεf does not depend on the radius,the critical conditions result in r F→∞for a cold outflow(Michel,1969,Li et al1992).Near the fast magnetosonic surface r∼σ1/3R L the MHD solution givesγ∼σ1/3,(64)εf∼σ−2/3.(65) Hence,Eqns.(53),(55),and(56)result inξr∼σ−2/3,(66)ξθ∼σ−2/3,(67)ξϕ∼σ−1/3.(68) As we see,theθ–component of the velocity plays no role in the determination of theγ.However,analyzing the left-hand sides of the Eqns.(23)–(28)one can evaluate the additional(nonhydrodynamic)varia-tions of the velocity components∆ξ±r∼λ−1σ−4/3,(69)∆ξ±θ∼λ−1σ−2/3,(70)∆ξ±ϕ∼λ−1σ−1.(71) Hence,for nonhydrodynamic velocities∆ξ±r≪ξr and∆ξ±ϕ≪ξϕto be small,it is necessary to have a large magnetizationparameterσ≫1only.On the other hand,∆ξ±θ/ξθ∼λ−1.In other words,for a highly magnetized plasmaσ≫1even outside the fast magnetosonic surface the velocity components(and,hence,the particle energy)can be considered hydrodynamically. The difference∼λ−1appears in theθcomponent only,but it does not affect the particle energy.Finally,one can obtain from (39),(40)thatδ−εftanθδ−σ−11∂θ+sinθξr.(75) Together with(21)one can obtain for r≫r Fγ=σ 2cosθεf−εsinθ∂f∂r r2∂f∂θξr+1∂θ(ξϕsinθ)=0.(77) Together with(76)this equation in the limit r≫r F coincides with the asymptotic version of the trans–field equation (Tomimatsu1994,Beskin et al1998)ε∂2f∂r−sinθD+1∂θ=0,(78)where g(θ)=K(θ)/sin2θ,andc 1999RAS,MNRAS000,1–??On the particle acceleration near the light surface of radio pulsars7D +1=1∂rr 2∂δ∂θ+1∂θ(ξϕsin θ)+2λ(ξ+r −ξ−r )=0.(80)Indeed,one can see from equations (19)and (20)that near the origin x =R s in the case γ+in =γ−in (and for the small variationof the current ζ∼σ−4/3which is necessary,as was already stressed,to pass through a fast magnetosonic surface)the densityvariation on the surface is large enough:(η+−η−)∼γ−2in ≫ζ.Hence,the derivative ∂2δ/∂r 2here is of the order of γ−2in .Onthe other hand,according to (22),the derivative ε∂2f/∂r 2is x 2times smaller.This means that in the two–component system the longitudinal electric field is to appear resulting in a redistribution of the particle energy.Clearly,such a redistribution is impossible for the charge–separated outflow.In other words,for a finite particle energy a one–component plasma cannot maintain simultaneously both the Goldreich charge and Goldreich current density (4).In a two–component system with λ≫1it can be realized by a small redistribution of particle energy (Ruderman &Sutherland 1975,Arons &Scharlemann 1989).For simplicity,let us consider only small distances x ≪1.In this case one can neglect the changes of the magnetic ing now (25)and (26),we haveγ+=γin −4λσδ;(81)γ−=γin +4λσδ.(82)Finally,taking into account that ξθand ξϕare small here,one can obtain from (20)r2∂2δ∂r +1∂θsin θ∂δγ2in,(83)where A =16λ2σ16λ2σ,(86)and µ≈√∂rr2∂δ∂θξr +1∂θ(ξϕsin θ)=0.(89)c1999RAS,MNRAS 000,1–??8V.S.Beskin and R.R.RafikovAsδ∼εf≪σ−2/3for r≪r F,andξr∼γ−20≫δ,thefirst term in(89)can be omitted.As a result,the solution of Eqn.(89)coincides exactly with the MHD expression,i.e.γ2=γ2in+x2sin2θ(54).Finally,using(87),(88),and(55)–(56), one can easily check that the nonhydrodynamical terms(47)in the trans–field equation(48)do actually vanish.4THE BOUNDARY LAYERLet us now consider the case when the longitudinal electric current I(R,θ)in the magnetosphere of radio pulsars is too small (i.e.the disturbance l(θ)is too large)for theflow to pass smoothly through the fast magnetosonic surface.First of all,it can be realized when the electric current is much smaller than the Goldreich one.This possibility was already discussed within the Ruderman–Sutherland model of the internal gap(Beskin et al1983,Beskin&Malyshkin1998).But it may take place in the Arons model(Arons&Scharlemann1979)as well.Indeed,within this model the electric current is determined by the gap structure.Hence,in general case this current does not correspond to the critical condition at the fast magnetosonic surface.In particular,it may be smaller than the critical current(of course,the separate consideration is necessary to check this statement).For simplicity let us consider the case l(θ)=h sin2θ.Neglecting now the last terms∝σ−1in the trans–field equation (48),we obtainε(1−x2sin2θ)∂2fx2∂sinθ∂f∂x−2εsinθcosθ∂f(2|h|)1/4.(92) As we see,for l(θ)=h sin2θthis surface has the form of a cylinder.It is important that the disturbance of magnetic surfaces εf∼(|h|)1/2remains small here.Comparing now the position of the light surface(92)with that of the fast magnetosonic surface(62),one canfind that the light surface is located inside the fast magnetosonic one ifσ−4/3≪|h|≪1,(93) which is opposite to(49).One can check that the condition(93)just allows to neglect the non force–free term in Eqn.(48).Using now the solution(91)and the MHD conditionδ=εf,one canfind from(58)2γ3−2σ hx2sin4θ+1√x0−x sinθ,(95) wherex0=14(2|h|)1/21On the particle acceleration near the light surface of radio pulsars 9 Figure1.The behavior of the Lorentz factor in the caseσ−4/3≪|h|≪1.One can see that the one–fluid MHD solution(95)existsforγ<σ1/3only.But in the two–fluid approximation in the narrow layer∆̟=̟c/λthe particle energy increases up to the value∼σcorresponding to the full conversion of the electromagnetic energy to the energy of particles.invariants(39)and(40)can be used to defineξ±ϕ:ξ+ϕ=1γ+ ;(99)ξ−ϕ=1γ− .(100)Furthermore,one can define2ξ+r=1(γ−)2+(ξ−ϕ)2+(ξ−θ)2.(102) As to the energy integral(38),it determines the variation of the currentζ.Now it can be rewritten asζ=22σsinθ.(103)Finally,Eqns.(19)–(28)look like̟2c d2δ2cosθ ξ+θ− λ+12cosθ ξ+r− λ+1d̟2=−2sin2θ λ−12cosθ ξ−ϕ ,(105)̟c d2σsinθ−̟ccosθd̟−sinθξ+r+sinθd̟ ξ−θγ− =−4λσ −γ++γ−sinθdδx0ξ−ϕ ,(107)̟cdd̟−sinθξ+θ,(108)c 1999RAS,MNRAS000,1–??10V.S.Beskin and R.R.Rafikov̟c dd̟−sinθξ−θ,(109)where we neglected the terms∝δ/r in(106)and(107).Comparing the leading terms,we have inside the layer∆̟/R L∼λ−1γ±∼h1/2cσ,(110)ξ±θ∼h1/4c,(111)ξ±r∼h1/2c,(112)∆δ∼h3/4c/λ,(113) where h c=|h|.Then the leading terms in(99)–(103)for∆̟>λ−1R L areξ+ϕ=1x0,(114)ξ−ϕ=1x0,(115)2ξ+r=(ξ+ϕ)2+(ξ+θ)2,(116) 2ξ−r=(ξ−ϕ)2+(ξ−θ)2,(117)ζ=−(γ++γ−)d̟2=2λsinθcosθ(ξ+θ−ξ−θ),(119)̟c d2σsinθ−̟ccosθd̟−sinθξ+r,(120)̟c d2σsinθ−̟ccosθd̟−sinθξ−r,(121)̟cdd̟ γ− =4λσsinθξ−θ,(123)with all the terms in the right–hand sides of(120)and(121)being of the same order of magnitude.As a result,the nonlinear equations(119)–(123)and(105)give the following simple asymptotic solutionγ±=4sin2θσ(λl)2,(124)ξ±θ=∓2sinθλl,(125)∆δ=−4On the particle acceleration near the light surface of radio pulsars11F(rad) x =−2m2c4γ2 (E y−B z)2+(E z−B y)2 ,(129)which can be important for large enough particle paring(129)with appropriate terms in(120)–(123)one can conclude that the radiation force can be neglected forσ<σcr,whereσcr= cc <3×10−3B−3/712λ2/74(131)which givesP>0.06B3/712λ−2/74s.(132)Hence,for most radio pulsars the radiation force indeed can be neglected.As to the pulsars withσ>σcr,it is clear that for γ>σcr the radiation force becomes larger than the electromagnetic one and strongly inhibits any further acceleration.As a result,we can evaluate the maximum gamma–factor which can be reached during the acceleration asγmax≈σcr≈106.(133)5DISCUSSIONThus,on a simple example it was demonstrated that for real physical parameters of the magnetosphere of radio pulsars (σ≫1andλ≫1)the one–fluid MHD approximation remains true in the whole region within the light surface|E|=|B|. On the other hand,it was shown that in a more realistic2D case the main properties of the boundary layer near the light surface existing for small enough longitudinal currents I<I GJ(effective energy transformation from electromagneticfield to particles,current closure in this region,smallness of the disturbance of electric potential and poloidal magneticfield)remain the same as in the1D case considered previously(Beskin et al1983).It is necessary to stress the main astrophysical consequences of our results.First of all,the presence of such a boundary layer explains the effective energy transformation of electromagnetic energy into the energy of particles.As was already stressed,now the existence of such an acceleration is confirmed by observations of close binaries containing radio pulsars(as to the particle acceleration far from a neutron star,see e.g.Kennel&Coroniti1984,Hoshino et al1992,Gallant&Arons 1994).Simultaneously,it allows us to understand the current closure in the pulsar magnetosphere.Finally,particle acceleration results in the additional mechanism of high–energy radiation from the boundary of the magnetosphere(for more details see Beskin et al1993).Nevertheless,it is clear that the results obtained do not solve the whole pulsar wind problem.Indeed,as in the cylindrical case,it is impossible to describe the particle motion outside the light surface.The point is that,as one can see directly from Eqn.(126),for a complete conversion of electromagnetic energy into the energy of particles it is enough for them to pass onlyλ−1of the total potential drop between pulsar magnetosphere and infinity.It means that the electron–positron wind propagating to infinity has to pass the potential drop which is much larger than their energy.It is possible only in the presence of electromagnetic waves even in an axisymmetric magnetosphere which is stationary near the origin.Clearly,such aflow cannot be considered even within the two–fluid approximation.In our opinion,it is only a numerical consideration that can solve the problem completely and determine,in particular,the energy spectrum of particles and the structure of the pulsar wind.Unfortunately,up to now such numerical calculations are absent.ACKNOWLEDGMENTSThe authors are grateful to I.Okamoto and H.Sol for fruitful discussions.VSB thanks National Astronomical Observatory, Japan for hospitality.This work was supported by INTAS Grant96–154and by Russian Foundation for Basic Research(Grant 96–02–18203).REFERENCESArons J.,Scharlemann E.T.,1979,ApJ,231,854Begelman M.C.,Li Z.-Y.,1994,ApJ,426,269Beskin V.S.,Gurevich A.V.,Istomin Ya.N.,1983,Soviet Phys.JETP,58,235Beskin V.S.,Gurevich A.V.,Istomin Ya.N.,1993,Physics of the Pulsar Magnetosphere,Cambridge Univ.Press,CambridgeBeskin V.S.,Kuznetsova I.V.,Rafikov R.R.,1998,MNRAS299,341c 1999RAS,MNRAS000,1–??12V.S.Beskin and R.R.RafikovBeskin V.S.,Malyshkin L.M.,1998,MNRAS298,847Bogovalov S.V.,1997,A&A,327,662Djorgovsky S.,Evans C.R.,1988,ApJ,335,L61Gallant Y.A.,Arons J.,1994,ApJ,435,230Goldreich P.,Julian,W.H.,1969,ApJ,157,869Henriksen R.N.,Norton J.A.,1975,ApJ,201,719Heyvaerts J.,1996,in Chiuderi C.,Einaudi G.,ed,Plasma Astrophysics,Springer,Berlin,p.31Hoshino M.,Arons J.,Gallant Y.A.,Langdon A.B.,1992,ApJ,390,454Kennel C.F.,Coroniti,F.V.,1984,ApJ,283,694Kulkarni S.R.,Hester J.,1988,Nature,335,801Li Zh.–Yu.,Chiueh T.,Begelman M.C.,1992,ApJ,394,459Mestel L.,1999,Cosmical Magnetism,Clarendon Press,OxfordMestel L.,Shibata S.,1994,MNRAS,271,621Michel F.C.,1969,ApJ,158,727Michel F.C.,1973,ApJ,180,L133Michel F.C.,1991,Theory of Neutron Star Magnetosphere,The Univ.of Chicago Press,ChicagoOkamoto I.,1978,MNRAS,185,69Ruderman M.A.,Sutherland P.G.,1975,ApJ,196,51Shibata S.,1997,MNRAS,287,262Tomimatsu A.,1994,Proc.Astron.Soc.Japan,46,123c 1999RAS,MNRAS000,1–??。

Physics 20 - The Electromagnetic Spectrum 电磁波普

Physics 20 - The Electromagnetic Spectrum  电磁波普
kilometres per second.
The Electromagnetic Spectrum
Features of the electromagnetic
spectrum
1. They can travel through a vacuum (eg. Space) 2. In a vacuum they travel at a speed of 300 000
LEARNING OBJECTIVES
Core •Give a qualitative account of the
dispersion of light as shown by the action on light of a glass prism including the seven colours of the spectrum in their correct order Describe the main features of the electromagnetic spectrum in order of wavelength • State that all e.m. waves travel with the same high speed in a vacuum • Describe typical properties and uses of radiations in all the different regions of the electromagnetic spectrum including: – r adio and television communications (radio waves) – s atellite television and telephones (microwaves) – e lectrical appliances, remote controllers for televisions and intruder alarms (infra-red) – medicine and security (X-rays) • Demonstrate an awareness of safety issues regarding the use of microwaves and X-rays

微机电系统工程专业英语词汇

微机电系统工程专业英语词汇

微机电系统工程专业英语词汇微机电工程材料该课程介绍了微机电系统中常用的材料的性质、选择和应用,包括金属、半导体、陶瓷、聚合物等。

该课程涉及的专业英语词汇如下:中文英文微机电系统Microelectromechanical Systems (MEMS)材料Material性质Property选择Selection应用Application金属Metal半导体Semiconductor陶瓷Ceramic聚合物Polymer晶体结构Crystal structure晶格常数Lattice constant晶向Crystal orientation晶面Crystal plane点阵Lattice基元Primitive cell单位晶胞Unit cell晶界Grain boundary缺陷Defect掺杂Doping禁带宽度Band gap width载流子Carrier导电性Conductivity阻值Resistance应力Stress应变Strain弹性模量Elastic modulus泊松比Poisson's ratio热膨胀系数Thermal expansion coefficient热导率Thermal conductivity热容量Heat capacity熔点Melting point硬度Hardness韧性Toughness耐腐蚀性Corrosion resistance中文英文表面粗糙度Surface roughness表面处理Surface treatment氧化层Oxide layer沉积方法Deposition method微机电器件与系统该课程介绍了微机电系统中常见的器件和系统的原理、结构和功能,包括传感器、执行器、开关、滤波器、振荡器等。

该课程涉及的专业英语词汇如下:中文英文微机电器件与系统Microelectromechanical Devices and Systems (MEDS)原理Principle结构Structure功能Function传感器Sensor执行器Actuator开关Switch滤波器Filter振荡器Oscillator振动Vibration静电力Electrostatic force电容Capacitance电感Inductance电阻Resistance压电效应Piezoelectric effect热电效应Thermoelectric effect磁电效应Magneto-electric effect光电效应Photoelectric effect声波Acoustic wave表面声波Surface acoustic wave (SAW)布拉格反射器Bragg reflector共振腔Resonant cavity质量灵敏度Mass sensitivity频率响应Frequency response功率消耗Power consumption信噪比Signal-to-noise ratio (SNR)线性度Linearity稳定性Stability可靠性Reliability微机械学该课程介绍了微机械系统的基本理论和方法,包括微尺度下的力学、流体力学、热力学、电磁学等。

2012-3-SOURCES

2012-3-SOURCES
F F 1 F 2 C aF x 22 C aF x 224 C a F 32 x fo rax
Resisting this force is the tension in the string which is, 2Tsinf = 2Tx/L
Hence, the equation of motion of the mass, m is
lower part of the cavity. Faster whirl will not give the oil enough time and the oil film will break. This occurs at
TMF = Number of Teeth x Order
Frequency Ranges2
High-frequency range components --Rolling-element bearings (anti-friction bearings): Ball and roller bearings exhibit cracks, corrosion pits on inner race, outer race,. --Frequencies up to 50 x order.
The area of the lower half of the film increases at a rate of
vD = f•2pD where D is the diameter of the journal.
Oil Whirl4
Slow whirling will give the oil enough time to fill the
Electromagnetic excitation1
In electro-machineries, the electromagnetic field will exert a force on the rotor. If the forces are not well balanced, then the rotor will be subjected to a net force that will set it into vibration.

从电磁的角度 英文

从电磁的角度 英文

从电磁的角度英文Electromagnetic PerspectiveElectromagnetism, a branch of physics that deals with the relationship between electricity and magnetism, plays a pivotal role in our understanding of how the universe works. Electromagnetic fields, generated by charged particles, are responsible for a wide range of phenomena, from the operation of electronic devices to the interactions between celestial bodies.From an electromagnetic perspective, the universe can be seen as a vast, interconnected web of energy. Electromagnetic waves, such as light and radio waves, propagate through space, carrying information and energy. These waves interact with matter, causing changes in the state of the matter and vice versa. For example, when light waves interact with atoms, they can cause electrons to transition between different energy levels, resulting in the absorption or emission of light.Electromagnetic fields are also responsible for the operation of many of our modern technologies. Electric motors, generators, transformers, and even computers rely on the principles of electromagnetism to function. The flow of electric current through wires generates magnetic fields, and vice versa. This interaction allows us to convert electrical energy into mechanical energy and vice versa, enabling a wide range of applications.Moreover, electromagnetism plays a crucial role in the communication systems that connect people across the globe. Radio waves, microwaves, and infrared radiation are all examples of electromagnetic radiation that we use to transmit information. From cell phones to satellites, our ability to communicate depends on the electromagnetic properties of matter and radiation.In conclusion, an electromagnetic perspective offers a deep and comprehensive understanding of the universe and the technologies that we rely on daily. It reveals the interconnectedness of all phenomena, from the smallest particles to the largest galaxies, and the intricate dance between electricity and magnetism that underliesall of these phenomena.。

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dences of each term. In order to study the violations of the isospin symmetry, the
electromagnetic effects Πem(q2) should also be written in the framework of the op-
ln
−q2 µ2
1 + q4 (mu
d¯d
1 + md u¯u ) + 12q4
αs G2 π
+
8 9q6
gs2
u¯u
d¯d

8 81q
6
gs2(
u¯u
2
+
d¯d 2)
+
7 27q6
e2eued(
gauge invariant.
3
Following the procedure in Ref. [8], there are additional Feynman diagrams shown
in Fig.2 for the charged current so that the Π±em(q2) for the charged qq¯ systems is
= Π(q2)(qµqν − q2gµν ) + Π1(q2)qµqν ,
(1)
where
Jµ(x) = q¯1(x)γµq2(x).
(2)
The Π(q2) in Eq. 1 can be written as
Π(q2) = Π0(q2) + Πem(q2) ,
(3)
where Π0(q2) is the leading term, and Πem represents the contributions from the electromagnetic effects. The quantity Π0(q2) has been evaluated in the literature. Thus we extend the results of Π0(q2) in Refs. [2, 7] by including the flavor depen-
2
of our studies[9] in the heavy-light quark systems are in good agreement with the available data. The focus of this paper is to extend our early studies to the light-light quark systems, such as the π and ρ systems.
The isospin symmetry breakings of pions have been discussed extensively in the chiral perturbation theory, in which the electromagnetic effects are shown to be dominant in the mass splittings of pions. Thus, a consistent treatment of the electromagnetic effect is particularly important for the isospin symmetry breakings in the qq¯, q = u or d, systems. In comparison with hadronic quark models, the QCD sum rule method for calculating isospin splittings has the advantage that one can directly use QED field theory rather than rely on models to estimate Coulomb corrections. In Ref. [8], a systematic approach for the electromagnetic effects in the operator product expansion for the qq¯ systems has been developed, in which the problem of the gauge invariance for the charged qq¯ states was resolved. This enables us to investigate the violations of the isospin symmetry due to all three effects, the nonperturbative effects, the quark mass differences and the electromagnetic effects, consistently in the QCD sum rule method. The nonterturbative effect is due to the difference of the quark condensate, which arises from the up and down quark mass difference. The results
quark condensates, of which the Feynman diagrams are shown in Fig. 3 and Fig. 4.
We present the expressions for Π(q2)
Πρ±
=

1 4π2
(1
+
αs ) ln π
−q2 µ2

1α 4π2 eued π
arXiv:hep-ph/9703371v1 20 Mar 1997
The Electromagnetic Effects In Isospin Symmetry Breakings Of qq¯ Systems
Shi-lin Zhu, and Zhenping Li Department of Physics, Peking University
diagrams are shown in Fig. 1. For the charge neutral current Π0em(q2), one could simply obtain the two-point functions by changing the gluons in QCD to the photons
PACS number(s): 13.40.Dk, 11.30.Hv, 12.38.Lg
1
The origin of mass differences in isospin multiplets has long been of great interest in nuclear and particle physics as a source of information about symmetry violations. Hadronic isospin violations are particularly important in that they arise from quark mass differences in Quantum Chromodynamics (QCD) (see Ref.[1] for a review of the early work in this area), and of course electromagnetic effects. Among the first applications of the method of QCD sum rules was the study of isospin violations in the ρ − ω system[2], in which it was recognized that the isospin splitting of the lightquark condensates can produce effects as large as the current-quark mass splittings and electromagnetic effects. Recently the QCD sum rule method has been used to study the neutron-proton mass difference[3, 4], the octet baryon mass splittings[5] and the mass differences in the charmed meson systems (the D and D∗ scalar and vector mesons)[6].
gauge invariant. Thus, the two point function Π±em(q2) for the charged qq¯ systems is
Π±em(q2)
=
Hale Waihona Puke −1 4π2
eq1
eq2
α π
ln
−q2 µ2
.
(5)
The leading nonperturbative terms due to the electromagnetic effects are the four
The basic approach of the QCD sum rule is to study the two-point correlation function in the Wilson operator product expansion (OPE), defined by
Π¯ µν (q2) = i d4xeiqx < T (Jµ(x)J¯ν (0)) >
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