QCD string in light-light and heavy-light mesons

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JLab JBuds Frames 耳机眼镜配套说明书

JLab JBuds Frames 耳机眼镜配套说明书

JBUDS FRAMESLocate the L & R on the back. If needed, add the Rubber Sleeves on hooks for narrow stem glasses.ASSEMBLY1Press and hold BOTH buttons 5+ seconds. One sidewill start blinking blue/white indicating ready to connect.CONNECTING BLUETOOTH1Slide the JBuds Frames on corresponding left and right stems of glasses.2Enter your device settings and connect to “JLab JBuds Frames”. Solid white lights will indicate you are connected.2C U S TOM ER S UPP OR TU.S .B A S E DWe love that you are rocking JLab!We take pride in our products and fully stand behind them.YOUR WARRANTYAll warranty claims are subject to JLab authorization and at our sole discretion. Retain your proof of purchase to ensure warranty coverage.CONTACT USReach out to us at ****************or visit/contactL I M I TE DT W O YEA R REGISTER TODAY/registerProduct updates | How-to tipsFAQs & moreThe JBuds Frames should be positioned closest to the ear for best performance.LRThin Frames:ICON facing out Very Thin Frames: LOGO facing outRubberSleevesADDING NEW/ADDITIONAL BLUETOOTH DEVICES:Turn OFF Bluetooth from any previously connected device. Turn ON Bluetooth enter Bluetooth pairing after 10 seconds. Select “JLab JBuds Frames” in new device settings to connect.VOICE PROMPTS“Hello”: Power ON“Earbuds joined”:Earbuds paired to each other“Ready to Pair”: JBuds Frames are ready to pair to Bluetooth device“Bluetooth Connected”:Earbud is connected to device “Battery Full”: 100-80%“Battery Medium”: 80-20%“Low Battery”: Less than 20%When power decreases to 10%,“Low Battery” will play“Goodbye”: Power OFFBUTTON FUNCTIONS Triple press either the right or left earbud 3 times for different EQ settings.EQ SETTINGSJLab SIGNATURE JLab C3™ signature sound with amplified bass and vocalsBASS BOOST Amplified bass and sub-bassCHARGINGRIGHT BUTTONLEFT BUTTONINDICATOR LIGHTINDICATORLIGHTVOLUME DOWN: Single pressSIRI (iOS) or “OK GOOGLE” (ANDROID):Double pressTRACK BACKWARD: Press & hold 1+ secVOLUME UP: Single pressPLAY / PAUSE: Double press TRACK FORWARD: Press & hold 1+ sec ANSWER: Single pressHANGUP: Double pressREJECT INCOMING CALLS: Press & hold 1+ secEQ CHANGE: Triple press on either earbud (Cycles JLab Signature/Bass Boost)POWER ON / OFF:Press & hold 3+ sec on either earbud (Button will power OFF both sides)ORConnect the JBuds Frames to computer or USB 5V 1A (or less) output device.CHARGINGQUICK TIPS, Press and hold both buttons 15+ sec..Press and hold both buttons 3+ sec to power ON. JBuds Frames will start blinking blue/white indicating ready to connect. Enter device settings and reconnect.Position the JBuds Frames as close to your ears as possible.This will greatly improve the audio performance.You can use either JBuds Frames left or right independently or both together with Dual Connect to listen to music or take calls. Note you will only have access to the left or right controls if you’re using only one.ORL R23CAUTIONS• Avoid extreme heat, cold, and humidity.• Avoid dropping or crushing the earbuds.• Wax may build up in the earbud tips, lowering the sound quality.Carefully remove the wax with a cotton swab or other small tool to improve the sound quality.• If you experience discomfort or pain, try lowering the volume or discontinuing use temporarily.• If you experience regular discomfort while using this product, discontinue use and consult your physician.• We recommend you treat your earbuds as you would a nice pair of sunglasses and keep them in safe location when not in use.Shop products | Product alerts | Burn-in your headphonesJLab Store + Burn-in Tool。

TP-Link 网络测试设备说明书

TP-Link 网络测试设备说明书

Before using the unit for the first time, do the following:y Turn the unit ON.y If the Power indicator is red, charge the battery.Status indicatorsThe indicators on the unit show the battery and network connect status, as follows:Power – Indicates the power or battery statusy Blinking green – Powering up or down y Solid green – Unit is ony Solid yellow – Battery remaining is less than 30%y Solid red – Battery remaining is less than 10%y Flashing red – Battery is very low and unit will shutdown soon Pair – Indicates the Bluetooth radio statusy Blinking – Waiting for pairingy Solid – Paired with the mobile device Service – Indicates the status of the service tests Network – Indicates the the status of the service testsLink – Indicates the status of the service tests Physical – Indicates the status of the physical layerSFP – Indicates the SFP+ port is the active port for the current test ETH – Indicates the ethernet port is the active port for the current testWiFi – Indicates the WiFi interface is the active interface for the current testCHG – Indicates the charge status. The indicator is off when the unit is not plugged in or charging.y Blinking orange – Charging, battery is less than 90% y Solid orange – Charging is almost complete y Solid green – Charge completey Flashing red – Error in charging or powering the unit. Make sure you are using the VIAVI charger supplied with the unit and try again.The meter may need to be serviced by a Certified Repair Center. Before sending in the unit for repair, contact VIAVI for an RMA.Power and Pair buttonsThe Power and Pair buttons are found near the top of the unit.Pair – Press to pair with a Bluetooth device Power – Press to turn the Companion on or off Play – Used for the Delayed Start testing feature. See the User’s Guide for more information.NSC-100Quick Start GuideBenefitsy Simply test everything anywhere – PON, Ethernet, WiFiy Verify true customer experience and physical network layer on all PON1, Ethernet, and WiFi test interfaces y Confirm PON service delivery is good before troubleshooting the premises y Share reports directly via emaily Drive compliance of both direct and contracted staff with centralized, cloudbased workflow and result managementFeaturesy GPON, XGSPON, Ethernet and WiFi tests, including throughput tests up to 2 Gbps y Ethernet 1G, 2.5G, 5G and 10G interfaces y 3x3 WiFi antenna with 2.4 & 5GHz y PON data analysis (PON-ID) y PON power levels y Job ManagerPreparation for useWhen you unpack the unit, do the following:y Inspect the unit for damage. If damaged, put back in box and contact VIAVI customer service (see the Technical Assistance section on the next page). y If undamaged, save the box and packing materials in case you need to ship the unit in the future.Power and Pair indicatorsService and Network indicatorsPower and Pair buttons Status indicatorsBottom viewEthernet port(10/100/1000 Mbps)USB-Ccharge portUSB 3.0 port (Type A)SFP+ optical port Protective rubber doorCharging the batteryConnect the supplied AC adapter to the USB-C port on the unit to power the Companion or charge the battery. A full charge could take up to an hour or so.Test modesThe Companion has a simplified test structure: OneCheck PON, OneCheck Ethernet, OneCheck WiFi, WiFi Expert, Loopback, TWAMP Light, and Fusion Client features toprovide autotests and troubleshooting via the VIAVI Mobile Tech app.Run OneCheck for comprehensive autotests of your network and access points. S elect a test from the Companion Main menu, then select a profile to test.Using the OneCheck dashboardOneCheck provides a comprehensive dashboard that shows results for Speedtests, Ping, Network, GPON, WiFi access Points, etc.For each panel inOneCheck, you can get more test result details by touching the panel.Pairing the Companion to your mobile deviceTo control the user interface of the Companion, the mobile device must be paired with the unit over Bluetooth.1.On the Companion, press and hold the Pairbutton for 3 seconds to enter pairing mode. The blue Pair indicator blinks.2.On the mobile device, do the following:y Go to the Settings menu, then select Bluetooth .y Verify that the device is not paired with any NSC-100 Companion unit.3.From the Mobile Tech Main menu, under My Devices , find the Companion, shown as “NSC-100”, and select Connect .If you don’t see the device, you may need to select Discover Devices .4. When the Companion is connected, the Pair indicator will be solid.5.On the mobile device, the Companion should be paired and the Main menu will now show the Companion menu.You can now control the instrument through the Mobile Tech app and run all tests on the Companion.© 2021 VIAVI Solutions Inc.Product specifications and descriptions in this document are subject to change without notice.22137285 July 2021EnglishVIAVI SolutionsNorth America 1.844.GO VIAVI / 1.844.468.4284Latin America +52 55 5543 6644EMEA +49 7121 862273APAC+1 512 201 6534All Other Regions/contacts***************************Mobile Tech Main menuIn the Main menu, you can see details of the instrument, run Companion tests, sync to StrataSync, manage files on the unit, and even view documentation.You’ll also see the date and time of the last time your meter synced to StrataSync.Near the top of the Main menu, you can select Show more to see details on your instrument, including all of the installed options.Using the Companion with a mobile deviceThe Companion is designed to be paired with a mobile device or tablet(such as an iPhone, iPad, or similar Android device), and leverages the user interface of those devices along with the VIAVI Mobile Tech app to provide a smooth user experience.You can view test results, set up the Companion, sync files, update the meter, and configure test parameters from the app.To get started, download the VIAVI Mobile Tech app from the App Store or Google Play.Connecting to StrataSyncYou can connect to StrataSync using your smartphone or tablet anytime, anywhere using the VIAVI Mobile Tech app.Once your instrument is connected to the Mobile Tech app via Bluetooth, geo locationinformation can be added to reports and files when syncing to StrataSync. If configuration files or work orders are set to be deployed from StrataSync to your meter, you can check those here, as well as browsing files from the unit itself.Once you download the application, log in to StrataSync just as you do on the website. To operate the tests, follow the instructions on the application screens.Mobile T echUsing the Mobile Tech appLogging in to StrataSyncTo get started using the Mobile Tech app, you need to log in to StrataSync.1. Launch the Mobile Tech app on your mobile device.2. Select the Login to StrataSync button. The Login screen will be displayed.3.Enter your Username and Password, then select the Sign In button. The Mobile Tech Main menu will be displayed.y – Run tests and configure profiles for the CompanionBefore doing any tests, you may need to set up profiles for your network. Companion > Profile y Job Manager – Attach jobs to tests, including customer info and work orders, and track test results y Instrument Sync – Sync your instrument to StrataSync and deploy configuration filesy NSC-100 Files and Mobile Tech Files – Manage the files on the unit you can save to your phone or tablet. Use the NSC-100 Files menu to manage filesstored on your meter, use the Mobile Tech Files menu to manage those stored on your mobile device. y Documentation – View and download various documentation for your instrument, including applications notes, software release notes, and quick reference guidesTechnical assistanceIf you require technical assistance, call 1-844-GO-VIAVI / 1.844.468.4284.For the latest TAC information, visit/en/services-and-support/support/technical-assistanceConnect buttonNSC-100。

ResearchObjectives

ResearchObjectives

Research ObjectivesThe MILC Collaboration is engaged in a broad research program in Quantum Chromodynamics (QCD).This research addresses fundamental questions in high energy and nuclear physics,and is directly related to major experimental programs in thesefields.It includes studies of the mass spectrum of strongly interacting particles,the weak interactions of these particles,and the behavior of strongly interacting matter under extreme conditions.The Standard Model of High Energy Physics encompasses our current knowledge of the funda-mental interactions of subatomic physics.It consists of two quantumfield theories:the Weinberg-Salaam theory of electromagnetic and weak interactions,and QCD,the theory of the strong interac-tions.The Standard Model has been enormously successful in explaining a wealth of data produced in accelerator and cosmic ray experiments over the past thirty years;however,our knowledge of it is incomplete because it has been difficult to extract many of the most interesting predictions of QCD,those that depend on the strong coupling regime of the theory,and therefore require non-perturbative calculations.At present,the only means of carrying out non-perturbative QCD calculations fromfirst principles and with controlled errors,is through large scale numerical sim-ulations within the framework of lattice gauge theory.These simulations are needed to obtain a quantitative understanding of the physical phenomena controlled by the strong interactions,to de-termine a number of the fundamental parameters of the Standard Model,and to make precise tests of the Standard Model’s range of validity.Despite the many successes of the Standard Model,it is believed by high energy physicists that to understand physics at the shortest distances,a more general theory,which unifies all four of the fundamental forces of nature,will be required.The Standard Model is expected to be a limiting case of this more general theory,just as classical mechanics is a limiting case of the more general quantum mechanics.A central objective of the experimental program in high energy physics,and of lattice QCD simulations,is to determine the range of validity of the Standard Model,and to search for new physics beyond it.Thus,QCD simulations play an important role in efforts to obtain a deeper understanding of the fundamental laws of physics.QCD is formulated in the four-dimensional space-time continuum;however,in order to carry out numerical calculations one must reformulate it on a lattice or grid.It should be emphasized that the lattice formulation of QCD is not merely a numerical approximation to the continuum formu-lation.The lattice regularization of QCD is every bit as valid as continuum regularizations.The lattice spacing a establishes a momentum cutoffπ/a that removes ultraviolet divergences.Stan-dard renormalization methods apply,and in the perturbative regime they allow a straightforward conversion of lattice results to any of the standard continuum regularization schemes.Lattice QCD calculations proceed in two steps.In thefirst,one uses importance sampling tech-niques to generate gauge configurations,which are representative samples from the Feynman path integrals that define QCD.These configurations are saved,and in the second step they are used to calculate a wide variety of physical quantities.It is necessary to generate configurations with a range of lattice spacings,and then perform extrapolations to the zero lattice spacing limit.Fur-thermore,the computational cost of calculations rises as the masses of the quarks,the fundamental constituents of strongly interacting matter,decrease.Until recently,it has been too expensive to carry out calculations with the masses of the two lightest quarks,the up and the down,set to their physical values.Instead,one has performed calculations for a range of up and down quark masses, and extrapolated to their physical values guided by chiral perturbation theory,an effectivefield theory that determines how physical quantities depend on the masses of the lightest quarks.The extrapolations in lattice spacing(continuum extrapolation)and quark mass(chiral extrapolation) are the major sources of systematic errors in QCD calculations,and both must be under control in order to obtain trustworthy results.In our current simulations,we are,for thefirst time,working at or near the physical masses of the up and down quarks.The gauge configurations produced in these simulations greatly reduce,and will eventually eliminate,the systematic errors associatedwith the chiral extrapolation.A number of different formulations of QCD on the lattice are currently in use by lattice gauge theorists,all of which are expected to give the same results in the continuum limit.In recent years, major progress has been made in thefield through the development of improved formulations(im-proved actions)which reducefinite lattice spacing artifacts.Approximately twelve years ago,we developed one such improved action called asqtad[1],which significantly increased the accuracy of our simulations for a given amount of computing resources.We have used the asqtad action to generate an extensive library of gauge configurations with small enough lattice spacings and light enough quark masses to perform controlled calculations of a number of physical quantities. Computational resources provided by the DOE and NSF have enabled us to complete our program of generating asqtad gauge configurations.These configurations are publicly available,and have been used by us and by other groups to study a wide range of physical phenomena of importance in high energy and nuclear physics.Ours was thefirst set of full QCD ensembles that enabled control over both the continuum and chiral extrapolations.We have published a review paper describing the asqtad ensembles and the many calculations that were performed with them up to2009[2]. Over the last decade,a major component of our work has been to use our asqtad gauge config-urations to calculate quantities of importance to experimental programs in high energy physics. Particular emphasis was placed on the study of the weak decays and mixings of strongly interact-ing particles in order to determine some of the least well known parameters of the standard model and to provide precise tests of the standard model.The asqtad ensembles have enabled the calcu-lation of a number of physical quantities to a precision of1%–5%,and will enable many more quantities to be determined to this precision in the coming years.These results are already having an impact on experiments in high energy physics;however,in some important calculations,partic-ularly those related to tests of the standard model,higher precision is needed than can be provided by the existing asqtad ensembles.In order to obtain the required precision,we are now working with the Highly Improved Staggered Quark(HISQ)action developed by the HPQCD Collabora-tion[3].We have performed tests of scaling in the lattice spacing using HISQ valence quarks with gauge configurations generated with HISQ sea quarks[4].We found that lattice artifacts for the HISQ action are reduced by approximately a factor of2.5from those of the asqtad action for the same lattice spacing,and taste splittings in the pion masses are reduced by approximately a factor of three,which is sufficient to enable us to undertake simulations with the mass of the Goldstone pion at or near the physical pion mass.(“Taste”refers to the different ways one can construct the same physical particle in the staggered quark formalism.Although particles with different tastes become identical in the continuum limit,their masses can differ atfinite lattice spacing).More-over,the improvement in the quark dispersion relation enables us to include charm sea quarks in the simulations.The properties of the HISQ ensembles are described in detail in Ref.[5],and the first physics calculations using the physical quark mass ensembles in Refs.[6,7,8].The current status of the HISQ ensemble generation project is described at the link HISQ Lattice Generation and some initial calculations with them at Recent Results.The HISQ action also has major advan-tages for the study of QCD at high temperatures,so we have started to use it in our studies of this subject.Projects using the HISQ action will be a major component of our research for the next several years.Our research is currently focused on three major areas:1)the properties of light pseudoscalar mesons,2)the decays and mixings of heavy-light mesons,3)the properties of strongly interacting matter at high temperatures.We briefly discuss our research in each of these areas at the link Recent Results.References[1]The MILC Collaboration:C.Bernard et al.,Nucl.Phys.(Proc.Suppl.),60A,297(1998);Phys.Rev.D58,014503(1998);G.P.Lepage,Nucl.Phys.(Proc.Suppl.),60A,267(1998);Phys.Rev.D59,074501(1999);Kostas Orginos and Doug Toussaint(MILC),Nucl.Phys.(Proc.Suppl.),73,909(1999);Phys.Rev.D59,014501(1999);Kostas Orginos,Doug Tou-ssaint and R.L.Sugar(MILC),Phys.Rev.D60,054503(1999);The MILC Collaboration:C.Bernard et al.,Phys.Rev.D61,111502(2000).[2]The MILC Collaboration: A.Bazavov et al.,Rev.Mod.Phys.82,1349-1417(2010)[arXiv:0903.3598[hep-lat]].[3]The HPQCD/UKQCD Collaboration: E.Follana et al.,Phys.Rev.D73,054502(2007)[arXiv:hep-lat/0610092].[4]The MILC Collaboration: A.Bazavov al.,Phys.Rev.D82,074501(2010)[arXiv:1004.0342].[5]The MILC Collaboration: A.Bazavov al.,Phys.Rev.D87,054505(2013)[arXiv:1212.4768].[6]The MILC Collaboration: A.Bazavov et al.,Phys.Rev.Lett.110,172003(2013)[arXiv:1301.5855].[7]The Fermilab Lattice and MILC Collaborations:A.Bazavov,et al.,Phys.Rev.Lett.112,112001(2014)[arXiv:1312.1228].[8]The MILC Collaboration:A.Bazavov et al.,Proceedings of Science(Lattice2013)405(2013)[arXiv:1312.0149].。

A320英文试题

A320英文试题

A320英文试题A320试题1. What is the purpose of the pack?To regulate basic temperature2. What is the function of each pack controller?To control the corresponding pack and flow control valve3. What is the purpose of the zone controller?To control zone temperature4. How is the basic temperature regulated by the Zone Controller?By using the lowest zone temperature demand.5. What is the function of the trim air valve?To optimize the zone temperature by adding hot air6. What is the main purpose of the anti-ice valve?To stop ice formation across the pack condenser7. What is the purpose of the bypass valve?To modulate the pack discharge temperature8. What is the purpose of the RAM AIR flaps?To modulate the main airflow through the heat exchangers9. What flow is delivered by the pack with the PACK FLOW selector on LO and bleed airsupplied by the APU?High10. What happens when the RAM AIR pushbutton is set to ON?The emergency rain air inlet flap opens.11. What is the number of outflow valves and safety valves?One outflow valve and two safety valves12. What happens when manual mode is used?The outflow valve can be manually controlled to adjust the cabin altitude.13. What is the purpose of the safety valves?To prevent excessive positive and negative differential pressure14. Where do you check the correct Manual landing elevation setting?On the ECAM CAB PRESS page.15. What happens if the MODE SELECTOR is set to MAN and the DITCHINETpushbutton is set on?Only the outflow valve is not automatically controlled to close.16. Where does the LAV and GALLEYS ventilation air come from?From cabin distribution ducts17. What is the purpose of the Avionics Equipment Ventilation Computer?To ensure control and monitoring of the avionics ventilation system18. What is the purpose of the avionics ventilation system in the avionics bay?To ventilate the avionics equipment19. How is the fwd cargo compartment ventilated?With cabin ambient air20. What are the basic functions of the FACs?Rudder control and flight envelope protection21. Where are the FMGC functions controlled from?The FCU and MCDUs.22. When is FD engaged?As soon as electrical power is available23. Concerning AP engagement, which of the following is true?During the approach phase, it is recommended to engage the second AP.24. What is the purpose of the RMPs?To enable the frequencies of all the radio communication systems to be selected25. What is the purpose of the AMU?To act as an interface between the users and the various radio communication and radio navigation systems.26. What happens if RMP 2 fails?All communication frequencies can be controlled.27. What is the function of the AMU?It integrates all the crew communication functions.28. What is displayed in case of a SELCAL call on VHF 2?CALL light flashes amber on the VHF 2 key.29. Is it possible to transmit simultaneously on Passenger Address and VHF channels?NO30. What is the function of the RESET key?The RESET key is used to cancel all the lighted calls.31. How is the SELCAL CALL light reset?By pressing the RESET key on any ACP.32. How is a ground mechanic to flight crew call indicated in the cockpit?The MECH light flashes on all ACPs and a buzzer sounds.33. What is the purpose of the static dischargers?It’s to discharge static electricity.34. What is the purpose of the CVR?To record crew conversations and communications35. Where is the PTP located?On the forward attendant station36. The static Inverter operates:When on batteries only37. AC ESS BUS is normally supplied by the:AC BUS 138. DC BAT BUS can be supplied by the:DC BUS 1, DC BUS 2 or batteries39. AC transfers enable AC buses:To be supplied by any generator or external power.40. Which cabin panels are removable?All the panels41. Where are passenger oxygen masks stored?In the Passenger Service Unit42. Where are the cabin depressurization doors mounted?On the lower sidewall panels43. Where is the inflation reservoir of the escape slide of emergency exit located?In the cargo compartment44. Smoke hoods are supplied for the cabin attendants to:Flight a fire or against emission of smoke or noxious gases.45. Where are the rapid decompression panels installed?In the cutouts of the ceiling panels and lateral right sidewall linings46. How many Unit Load Devices (ULDs) can be loaded in the FWD Cargo compartmentif the Cargo Loading System is installed?With 3 ULDs47. Is the extinguishing system controlled by the FDU? NO48. Where are the fire detectors located?On the pylon, the fan and the core.49. The agent pushbutton is active when:Engine fire pushbutton is released out.50. What does the TEST pushbutton check?Both simultaneously.The fire detection loops A and B, FDU, indications and warnings.The squib circuit continuity of AGENT 1 and 2.51. How is an APU fire on ground normally extinguished?Automatically.52. How can a thermal discharge of the bottle be detected on a cold aircraft?By the red disc indicator53. How many fire detectors does the APU fire detection system comprise?Two54. How can the avionic smoke detector be tested?By a manual test from the CFDS55. Which warning lights are triggered in case of an avionics smoke detection?GEN 1 LINE SMOKE and BLOWER and EXTRACT FAULT lights.56. How are the smoke detectors connected to the SDCU?In a loop57. How many smoke detectors are installed in the Cargo compartments?Six58. When the test pushbutton is pressed and held, which conditions are simulated?Both Smoke and Bottle pressure drop.59. Lavatory fire extinguishing is performed by:Portable extinguisher60. Which surfaces are used for lift dumping?All spoilers.61. Which surfaces are used to control the roll?Ailerons and spoilers 2 to 562. Which surfaces can be mechanically controlled?Rudder and THS63. In normal conditions, what are the active protections in flare mode?Bank angle and stall protections64. What are the active protections in direct laws?No protection.65. What happens when both sticks are moved in the same or opposite direction?The surface movement is proportional to the algebraic sum of the deflection of both side sticks.66. How is it possible to inhibit the output of the other stick?By pressing in the take over pushbutton.67. What happens if the take over pushbutton of one stick is pressed in for more than 40seconds?The other stick remains deactivated after the take over pushbutton is released.68. How can a deactivated stick be reactivated?By a momentary action on the take over pushbutton of any side stick69. What are the consequences of one flap PCU motor inoperative?The flap surfaces extend (retract) at half speed.70. What happens when S/F configuration is 1+F and the CASreaches 210 knots?Flaps retract automatically to 0 and the new S/F Configuration is 171. Which tanks are the main supply tanks?Center tank and inner cells72. The Fuel Quantity Indicating System comprises:One FQIC and two FLSCUs73. What is the maximum total fuel capacity?41 736 lbs (18932 kg)74. Are wing tank pumps running while center tank is supplying?Yes, wing tank pumps are always running.75. The Engine LP Valve closes when:The engine is shut down or the ENG FIRE pushbutton is released out.76. When there is a low level in one inner cell:Two Transfer Valves, one in each wing, open.77. The inner cell is refueled only when:Outer cell is full.78. Refuel valves may be actuated:Electrically or manually79. Which hydraulic systems are pressurized by an engine driven pump?Green and Yellow.80. In normal operation, what is the blue Hydraulic system pressurized by?An electric pump81. Is it possible to stow the Ram Air Turbine in flight? No82. Can the Ram Air Turbine be extended automatically on ground? No83. What happens if the hydraulic pressure drops?The priority valves give priority to the essential systems.84. A blue system pipeline is identified by:A blue band and number 285. What happens in case of loss of electrical power supply to the engine anti-ice valve?The valve opens when the engine is running86. What happens in case of insufficient air pressure to the engine anti-ice valve?The valve closes as it is spring loaded closed.87. With both engine anti-ice pushbuttons set to ON, does the N1 limit change? YES88. When is the TAT probe heated?In flight, not on ground89. When is the pitot probe heated?Normal heating in flight, low heating on ground90. What happens in case of a WHC failure?The heating of the related side is lost.91. What happens when the EIU power supply circuit breakers are pulled?The windshield and windows are heated.92. How is each wiper controlled?By a three or four position rotary selector93. How do you perform a complete test of drain mast heating system?Both From PTP and From test pushbutton of the CU.94. How many levels of ice detection are provided? Two95. When is the ice detection system inhibited?On ground, below 1500 feet or TAT>8℃96. On which display are the engine parameters? E/W.97. What do the visual attention getters consist of?A red and an amber light in front each pilot.98. Which computer processes the warnings? FWC99. What is the basic role of the DMCs?They compute and generate displays.100. A ccording to these cockpit indicators:The Captain’s ND and PFD are not in normal configur ation.101. A ccording to these cockpit indications:The Captain’s PFD Display Unit is inoperative.102. W here does a warning message appear?Left memo area.103. W hat does a Warning message replace?Memos104. W hich ECAM page is displayed in cruise?CRUISE Page105. W hich ECAM page is displayed when the landing gear is selected down in phase 6?WHEEL page.106. O n which display does the warning message appear?ENGINE/WARNING display.107. W hat happens if the recall pushbutton is pressed?The warnings are recalled.108. W hat is displayed on the status page?Operational status messages109. T he clock provides UTC to:The CEDIU, FDIU and the two FMGCs.110. T he POST FLIGHT REPORT is made up from:The LAST LEG ECAM REPORT and the LAST LEG REPORT.111. W hich action must be taken by maintenance personnel when a class 1 failure affects an aircraft system?Refer to the MEL to know if the failure is a GO, NO GO or GO IF item.112. W hen does a class 3 failure has to be corrected?Class 3 failures can be left uncorrected.113. I n flight, a class 2 failure has occurred. Now, we are ground, where is this failure displayed?In the LAST LEG REPORT, the AVIONICS STATUS and the ECAM STATUS page.114. W hich Centralized Fault Display System functions are available in flight?CURRENT LEG REPORT, CURRENT LEG ECAM REPORT115. W hen you make a print of the PREVIOUS LEGS REPORT?You print only the page displayed on the Multipurpose Control and Display Unit (MCDU), even if the report contains several pages.116. W hich Centralized Fault Display System functions are available in BACKUP mode on ground?SYSTEM REPORT / TEST for main systems.117. (m) implies:A maintenance procedure described in the MMEL118. C ompared with the Airbus MMEL, an airline MEL can be:More restrictive119. W hich item is used if several task numbers are relative to a same “WARNING / MALFUNCTION” and “CFDS FAULT MESSAGE” association?The IDENTOFIERS item120. W hich are the main functions of the AIDS?Engine condition, APU condition and aircraft performance monitoring121. H ow does the AIDS operate?Manually through the MCDU and automatically through the DMU122. T he line, providing manual start and stop as well as status indication of the DAR, is displayed at the bottom of the AIDS MCDU menu page if:Both a DAR is installed and the DMU is equipped with a PCMCIA interface123. W hich hydraulic system powers normal landing gear operation?Green system124. W hich hydraulic system powers the nose wheel steering?Green system125. W hen does the UNLK light come on?When the gear is not locked in the selected position126. W hich hydraulic system powers normal braking?Green system127. H ow is inflight braking initiated?By setting the landing gear to the “UP” position128. I n case of normal braking system failure, how is alternate braking applied?As soon as the brake pedals are pressed in129. H ow can the parking brake be hydraulically powered?Either by yellow high pressure or by the brake accumulator 130. W hat is the maximum nose wheel steering angle obtained by the hand wheels?±74 degrees131. I s nose wheel steering available after a landing gear gravity extension?NO132. W here is the tire pressure indication displayed?On ECAM133. I n electrical emergency configuration, which cockpit lights remain on?F / O dome light and LH CENTER lighting instrument panel134. W hich lighting includes fluorescent lamps and integral ballast units?Cabin lighting, entrance lighting and lavatory lighting135. W ith the RWY TURN-OFF switch set to ON, when are the RUNWAY TURN-OFF lights on?When the Nose Landing Gear is down locked136. W hen is the emergency lighting system supplied by the EPSUs integrated batteries?When the EMER LIGHT pushbutton on the FAP is pressed and the 28 V DC ESS BUS is lost137. C an VOR 2 frequency be charged through RMP 1?NO 138. I n back-up mode an ILS can be tuned through:RMP1 or 2139. F rom which ADIRU can the DDRM1 receive information?ADIRU 1 or 3140. W hich ADIRU does not supply the DMC 1?ADIRU 2141. H ow do Pitot and static probes supply the ADIRUs?Using ADMs which convert pressure into digital format142. W here does ADIRU 3 receive TAT information from?Captain TAT sensor143. W hich pressure line(s) need(s) to be drained?Only the standby static line144. T he satellite orbital planes have an inclination of:55o to the Equator145. T he control segment is composed of:4 monitor stations and one master control station146. W hich aircraft are detected by the TCAS?ATC equipped A/C147. T he crew oxygen system consists of:A fixed cylinder with masks and a breathing hood system148. C an the cylinder pressure be checked when there is no electrical power?Yes149. W hat indicates an overboard discharge?A yellow indicator150. D oes the APU bleed valve opening have priority over the engine bleed valves opening?Yes151. W hat is the main function of the APU?To produce independent pneumatic and electrical power152. W hich component controls and monitors the APU?The Electronic Control Box153. T he Electronic Control Box has:Full authority over APU operation154. F rom where can an APU emergency shut down be performed?External power control panel155. N ormal APU shutdown is performed from?APU control panel156. W hat is the main function of the APU?To produce independent pneumatic and electrical power157. W hich component controls and monitors the APU? The Electronic Control Box158. The passenger door is maintained parallel to the fuselage by: The guide arms159. H ow is the operator warned, when there is a residual pressure in the cabin?By a red flashing light160.What does the green light fitted near the manualselector valve indicate?The door is fully open and locked.161.What directly provides the closure of the HP fuel shut off valve?The master lever to OFF position162.Which valve ensures the adequate fuel flow?The fuel metering valve.163.When does the fuel return valve open?When the engine oil temperature exceeds 93℃(200℉)164.When does the generator supply the ECU?When N2 is greater than 12%.165.Where is the TLA signal directly sent to? The ECU166.Why does the ECU interface directly with the FMGC?To send thrust parameters for autothrust function.167. What happens if the channel A fails?The ECU switches from the faulty channel to the channel B.168. What provides the selection of the igniters A/B? The ECU 169. What happens in manual mode when N 2 reaches 50%?Start valve is automatically closed.170. What causes an automatic continuous relight by FADEC?Flame-out detected.171.The Variable Bleed Valves are controlled by: The ECU172. What provides the HP rotor heating?The RACC system.173.What provides the ECU cooling in flight?Air inlet scoop174.What is the logic of the reverse operation?TLA position + Aircraft on ground + N2(engine running).175.Reverser system actuation is provided by two solenoid valves which are controlled from the: Engine Control Unit176.What does the CFDIU simulate during the MCDU reverse test? The N2.177. What happens if the oil supply filter is contaminated?The visual clogging indicator on the filter becomes red.178. What protects the scavenge pumps from metallic particles?Four magnetic chip detectors with stainers.179.What maintains the oil temperature within limits?The engine fuel/oil cooler and servo fuel heater180. To which temperature is the engine flat rated?ISA + 15℃(59℉)181. How is the thrust rating defined on the CFM56-5B?By an engine data programming plug182. An oil tank access is provided for servicing: On the left side fan cowl door183. A starter valve access panel is provided for manual operation:On the right side fan cowl door184. How is the accessory gearbox driven?By the HP rotor via the transfer gearbox185. What bearings support the HP rotor?N°3(dual bearing) and N°4186. The aerody namic station N°3 is: The HP compressor discharge187. What is the purpose of the Fuel Return Valve in the recirculation system? To maintain IDG oil, engine oil and fuel temperature within limits.188. What happens when the ENG MASTER lever is set to OFF?Both LP and HP fuel shut-off valves are closed.189. What does the FADEC consist of?The ECU and its peripherals, per engine190. In case of input loss, what happens?The channel in control uses valves from the other channel.191. If both windings of a torque motor fail, what happens?Control goes to a fail-safe position.192. If one winding of a torque motor fail, what happens?Switch over to the other channel.193. How does the starter operate? Pneumatically194. In which case can the EDU abort the start?Automatic start only195. Of which type is the ignition system?High voltage, high energy196. Which unit supplies servo pressure to the VSV actuators?The hydromechanical unit197. What is used to cool the fan and core compartments?Ram air for the fan compartment and fan air for the core compartment.198. Which air is used to feed the HPTACC system?HP compressor 4th and 9th stage air199. Where are located the engine controls?On the overhead panel and the center pedestal.200. Where are permanently displayed the engine primary parameters?On the ECAM upper display201. What is the purpose of the ENGINE MASTER switch?Both to open or close the HP fuel shut-off valve and to command and reset the FADEC functions.202. Which computer controls the engine thrust, either in manual mode or autothrust mode?ECU203. What is the normal cruise detent point?CL204. When is it possible to operate the thrust reverser system?On ground only.205. How is the thrust reverser actuated?Hydraulically.206. How is the Hydraulic Control Unit controlled?By the reverser lever through the ECU207. What happens when the main oil filter is clogged?The oil flows through the bypass valve and the backup filter.208. What does the master chip detector do in case of metal particles detection?It operates a visual indicator for ground inspection.。

用QCD因子化方法研究B→PV两体弱衰变过程

用QCD因子化方法研究B→PV两体弱衰变过程

第26卷 增刊 高能物理与核物理V o1.26,Supp. 2002年12月HIGH ENERGY PHYSICS AND NUCLEAR PHYSICS Dec.,2002 Two-Body B Decays to Pseudoscalar and Vector Mesonsin QCD Factorization ApproachYANG Mao-Zhi1 YANG Ya-Dong21 (Institute of High Energy Physics, CAS, Beijing 100039, China)2 (Department of Physics, Technion, Haifa 32000, Israel)Abstract Motivated by recent CELO measurements and the progress of the theory of B decays,B→PV(P=π, K; V= K*, ρ, ω) decay modes are studied in the framework of QCD factorization.All the measured branching ratios are well accommodated in the reasonable parameter space andpredictions for other decay modes are well below the experimental upper limits.Key words factorization, weak decay, mesonB physics is one of the most important fields nowadays because it is of great help for testing the quark flavor mixing theory of the standard model and exploring the source of CP violation. Most of the theoretical studies of B decays to pseudocalar and vector final states are based on the popular Naive Factorization approach[1]. As it was ponited out years ago in Ref. [2], the dominant contribution in B decays comes from the so-called Feynman mechanism, where the energetic quark created in the weak decay picks up the soft spectator softly and carries nearly all of the final-state meson's momentum. It is also shown that Pion form factor in QCD at intermediate engery scale is dominated by Feynman mechanism[3—5]. From this point, we can understand why the naive factorization approach have worked well for B and D decays, and the many existing predictions for B decays based on naive factorization and spectator ansatz do have taken in the dominant physics effects although there are shortcommings. However, with the many new data available from CLEO and an abundance of data to arrive within few years from the B factories BaBar and Belle, it is demanded highly to go beyond the naive factorization approach.Recently, Beneke et al., have formed an interesting QCD factorization formula for B exclusive nonleptonic decays[6,7]. The factorization formula incorporates elements of the naive factorization approach (as leading contribution) and the hard-scattering approach (as subleading corrections), which allows us to calculate systematically radiative(subleading nonfactorizable) corrections to naive factorization for B exclusive nonleptonic decays. An important product of the formula is that the strong final-state interaction phases are calculable, which arise from the2 高能物理与核物理(HEP &NP) 第26卷hard-scattering kernel and hence process dependent. The strong phases are very important for studying CP violation in B decays.The amplitude of B decays to two light mesons, say M 1 and M 2, is obtained through the hadronic matrix element <M 1(p 1) M 2(p 2)⏐O i ⏐B (p )>, here M 1 denotes the final meson that picks up the light spectator quark in the B meson, and M 2 is the another meson which is composed of the quarks produced from the weak decay point of b quark. Since the quark pair, forming M 2, is ejected from the decay point of b quark carrying the large energy of order of m b , soft gluons with the momentum of order of ΛQCD decouple from it at leading order of ΛQCD /m b in the heavy quark limit. As a consequence any interaction between the quarks of M 2 and the quarks out of M 2 is hard at leading power in the heavy quark expansion. On the other hand, the light spectator quark carries the momentum of the order of ΛQCD , and is softly transferred into M 1 unless it undergoes a hard interaction.Any soft interaction between the spectator quark and other constituents in B and M 1 can be absorbed into the transition form factor of B →M 1. The non-factorizable contribution to B →M 1 M 2 can be calculated through the diagrams in Fig.1.Fig. 1. Order αs non-factorizable contributions in B →M 1M 2 decays.The O i 's incorporated in Fig.1 are the operators in the effective Hamiltonian for B decays [8], ⎥⎥⎦⎤⎢⎢⎣⎡⎟⎟⎠⎞⎜⎜⎝⎛+++⎟⎟⎠⎞⎜⎜⎝⎛++=∑∑∑∑====21103g g ccqcb 21103g g uuq ub F eff2i i i i i i *i i i i i i *O C O C O C V V O C O C O C V V G H , (1)Where()()A V A V O --ββααu 1b u u q ⋅=, ()()A V A V O --αββαu 2b u u q ⋅=, ()()A V A V O --ββααc 1b c c q ⋅=, ()()A V A V O --αββαc 2b c c q ⋅=,()()AV A V O --ββq αα3q q b q ′′⋅=∑′,()()AV A V O --αβq βα4q q b q ′′⋅=∑′,()()AV A V O +′′′⋅=∑ββq αα5q q b q -, ()()A V A V O +′′′⋅=∑αβq βα6q q b q -, ()()A V A V e O +′′′′⋅=∑ββq q αα7q q b q 23-, ()()A V A V e O +′′′′⋅=∑αq q b q 23βq q βα8-,增 刊 杨茂志等:用QCD 因子化方法研究B →PV 两体弱衰变过程 3()()A V A V e O --ββq q αα9q q b q 23′′⋅=∑′′, ()()A V A V e O --αβq q βα10q q b q 23′′⋅=∑′′, ()()AA a g G b R m g O µνβαβµνλσ2/d π8/b 2s =. (2)Here q=d, s and (q'ε {u, d, s, c, b}), α and β are the SU (3) color indices and , A =1,...,8 are the Gell-Mann matrices, and denotes the gluonic field strength tensor. The Wilson coefficients evaluated at µ=m AαβλAG µνb scale are[8]C 1= 1.082, C 2=−0.185, C 3= 0.014, C 4=−0.035, C 5= 0.009, C 6=−0.041,C 7=−0.002/137, C 8=0.054/137, C 9=−1.292/137, C 10=0.262/137, C g =−0.143. (3) The non-factorizable contributions to B →M 1M 2 can be calculated through the diagrams in Fig.1. The details of the calculations can be found in Ref. [9]. In the numerical calculations we use[10]τ (B +) = 1.65×10-12s, τ (B 0) = 1.56×10-12s,M B = 5.2792GeV , m b = 4.8GeV , m c = 1.4GeV , f B= 0.180GeV , f π = 0.133GeV , f K = 0.158GeV , f K * = 0.214GeV , f ρ = 0.21GeV , f ω = 0.195GeV .For the chiral enhancement factors for the pseudoscalar mesons, we takeR π ±π= R K ±, 0 = -1.2 ,which are consistent with the values used in [6, 11, 12]. We should take care for R π0. As pointedout in Ref. [7], R π0 for π0 should be -2M /(m 2b (m u + m d )) and equal to R π± due to inclusion ofisospin breaking effects correctly.For the form factors, we take the results of light-cone sum rule[13,14]F B →π(0)=0.3, F B →K (0)=1.13F B →π(0), A =0.372, A =0.470,ρB 0→*K B 0→and assume (0)=1.2(0) since we find larger (0) is preferred by experimental data.ωB 0→A ρB 0→A ωB 0→A We take the leading-twist distribution amplitude (DA) φ(x ) and the twist-3 DA φ0(x ) of light pseudoscalar and vector mesons as the asymptotic form[15]φP,V (x ) =6x (1-x ), (x ) =1. (4) 0P φFor the B meson, the wave function is chosen as[16,17]()(),xM x x N x ⎥⎥⎦⎤⎢⎢⎣⎡=2B 22B 22B B 2exp 1ωφ-- (5)with ωB =0.4GeV , and N B is the normalization constant to make(x ) =1. φ∫1Bd φx B (x ) is stronglypeaked around x =0.1, which is consistent with the observation of Heavy Quark Effective Theory that the wave function should be peaked around ΛQCD /M B .We have used the unitarity of the CKM matrix V *uq V ub +V *V cq cb +V *tq V tb =0 to decompose the4 高能物理与核物理(HEP &NP)第26卷amplitudes into terms containing , V *uq V ub and V *V cq cb , and⏐V us ⏐=λ=0.2196, ⏐V ub /V cb ⏐=0.085±0.02, ⏐V cb ⏐=0.0395±0.0017, ⏐V ud ⏐=1-λ2/2 . (6) We leave the CKM angle γ as a free parameter.The numerical results of the branching ratios B →PV are shown in Fig.2 as the function of CKM angle γ. We can see from Fig. 2(a), (b) and (c) that for the three detected channels the predicted branching ratios agree well with the CLEO experiment data [18]. Our predictions for other decay modes are well below their 90% C.L. upper limits.There are several works available with detailed analysis of the CLEO new data of the decays of B to charmless PV states[11,12,19]. It is worth to note that the shortcomings in the “generalizedfactorization” are resolved in the framework of QCD Factorization. Nonfactorizable effects are calculated in a rigorous way here instead of being parameterized by effective color number. Since the hard scattering kernals are convoluted with the light cone DAs of the mesons, gluon virtualityk 2=2b m x in the penguin diagram Fig. 1(e) has well defined meaning and leaves no ambiguity as tothe value of k 2, which has usually been treated as a free phenomenological parameter in the estimations of the strong phase generated though the BSS mechanism [20]. So that CP asymmetries are predicted soundly in this approach. We present the numerical result of the branching ratios of B →PV decays in Table 1 with the relevant strong phases shown explicitly. It shows that the strong phases are generally mode dependent.Table 1. Strong phases in the branching ratios (in units of 10-6) for thecharmless decays modes studied by CLEO. (γ =Arg V *u b )B (B -→π-ρ0)=6.65⏐0.11e -i86.5°+e -i γ⏐2B (0B →π+ρ-)=19.79⏐0.11e i9.02°+e -i γ⏐2B (0B →π-ρ+)=13.43⏐0.03e i172°+e -i γ⏐2B (B -→π-ω)=10.59⏐0.065e i26.01°+e -i γ⏐2B (0B →π0ρ0)=0.11⏐0.21e 2.90°+e -i γ⏐2B (B -→π0ρ-)=10.81⏐0.176e i7.20°+e -i γ⏐2B (0B →π-ω)=1.49×10-3⏐1.64e i148°+e -i γ⏐2B (B -→K -ρ0)=0.55⏐0.24e -i162°+e -i γ⏐2B (B -→π-⎯K *0)=0.0012⏐56.4e -i15.7°+e -i γ⏐2B (B -→K -K *0)=0.030⏐2.86e i164°+e -i γ⏐2B (B -→π0K *-)=0.59⏐2.80e -i169°+e -i γ⏐2B (B -→K -ω)=0.80⏐0.48e -i9.23°+e -i γ⏐2B (0B →K 0ω)=0.72⏐0.81e -i 11.8°+e -i γ⏐2B (⎯B 0→K -ρ+)=0.96⏐0.63e -i7.20°+e -i γ⏐2B (0B →π0⎯K *0)=0.004⏐12.89e i67.61°+e -i γ⏐2Hou, Smith and W ürthwein have performed a model dependent fit using the recent CLEOdata and found γ =114degree. Using SU (3) flavor symmetry, Gronau and Rosner have analyzedthe decays of B to charmless PV final states extensively and found several processes are consistent with cos γ < 0. In this paper we find cos γ < 0 is favored by the B 2521+--→π-ρ0 and ⎯B 0→π-ρ++π+ρ- if their experimental center values are taken seriously. To meet its center value with cos γ < 0 , B -→π增 刊 杨茂志等:用QCD 因子化方法研究B →PV 两体弱衰变过程 5-ω would indicate larger form factor i.e. A (0) > A (0). In our numerical calculation, wehave taken A (0) = 0.446 which is still consistent with the LCSR results 0.372 ± 0.074ω→B 0ρ→B 0ω→B 0[13]. It isalso interesting to note that ⎯B 0→π+ρ- is suppressed by cos γ < 0 while ⎯B 0→π-ρ+ is enchanced. The defference between Br (⎯B 0→π+ρ-) and Br (⎯B 0→π-ρ+) is much more sensitive to γ than their sum.6 高能物理与核物理(HEP &NP) 第26卷Summarywe have calculated the branching ratios and CP asymmetries of the charmless decays B →PV(P = (π, K), V= (ρ,ω, K *)) in QCD factorization approach. We have used LCSR formfactors F B →π,K (0) and A (0) as inputs. The results of Br (B *K ,0ρ-→π-ρ0) and Br (⎯B 0→π±ρ) agree with CLEO m [18]very well and favor cos γ < 0 if their experimental center values are taken seriously. To meet its experimental center value and cos γ < 0, the decay B -→π-ω will prefer larger form factor (0). For the other decay modes, the branching ratios are predicted well below their 90% C.L. upper limits given in Ref. [18].ωB 0→A References1 Bauer M, Stech B, Wirbel M. Z. Phys., 1985, C29: 637; Z. Phys., 1987, C34: 1032 Chernyak V L, Zhitnitsky L R. Nucl. Phys., 1990, B345: 1373 Isgur N, Llewelyn-Smith C H. Phys. Rev. Lett., 1984, 52: 1080; Nucl. Phys., 1989, B317: 5264 Radyushkin A V . Acta Phys., 1984, Pol. 15: 4035 Stefanis N G . hep-ph/99113756 Beneke M, Buchalla G , Neubert M. Phys. Rev. Lett., 1999, 83: 19147 Beneke M, Buchalla G , Neubert M et al. hep-ph/00061248 Buchalla G , Buras A J, Lautenbacher M E. Rev. Mod. Phys., 1996, 68: 1125 9 YANG M Z, YANG Y Y . Phys. Rev., 2000, D62: 114019 10 Particle Data Group. Eur. Phys. J., 1998, C3: 1 11 CHENG H Y , YANG K C. hep-ph/991029112 HOU W S, Smith J G , W ürthwein F W. hep-ex/9910014 13 Ball P, Braun V M. Phys. Rev., 1998, D58: 094016 14 Ball P. JHEP09, 005(1998)15Lepage G P, Brodsky S J. Phys. Lett., 1979, B87: 359; Chernyak V L, Zhitinissky A R. Phys. Rep., 1983, 112: 173; Braun V M, Filyanov I E. Z. Phys., 1990, C48: 239 16 Keum Y Y , LI H -N, Sanda A I. Phys. Lett., 2001, B504: 2; Phys. Rev., 2001, D63: 054008 17 LÜ C D, Ukai D, YANG M Z. Phys. Rev., 2001, D63: 07400918 CLEO Collaboration. CLEO CONF 99-13; CLEO Collaboration. CLNS 99/1652 and CLEO 99-19 19 Gronau M, Rosner J L. Phys. Rev., 2000, D61: 073008 20Bander M, Silverman D, Soni A. Phys. Rev. Lett., 1979, 43: 242增刊杨茂志等:用QCD因子化方法研究B→PV两体弱衰变过程7 用QCD因子化方法研究B→PV两体弱衰变过程杨茂志1 杨亚东21 (中国科学院高能物理研究所北京 100039)2 (Department of Physics, Technion, Haifa 32000, Israel)摘要基于最近CLEO实验和B介子物理中理论研究的进展, 在QCD因子化方案下研究了B介子到一个赝标π, K和一个矢量介子ρ, ω的两体弱衰变过程.在合理的参数范围内, 理论计算与实验相符得很好.关键词因子化弱衰变介子。

Spectrum of light scattered from a deformed Bose-Einstein condensate

Spectrum of light scattered from a deformed Bose-Einstein condensate

a r X i v :q u a n t -p h /9907084v 1 26 J u l 1999Spectrum of light scattered from a “deformed”Bose–Einstein condensateStefano Mancini †and Vladimir I.Man’ko ‡†Dipartimento di Fisica and Unit`a INFM,Universit`a di Milano,Via Celoria 16,I-20133Milano,Italy ‡P.N.Lebedev Physical Institute,Leninskii Prospekt 53,Moscow 117924,Russia (Date:May 25,1999)Abstract The spectrum of light scattered from a Bose–Einstein condensate is studied in the limit of particle-number conservation.To this end,a description in terms of deformed bosons is invoked and this leads to a deviation from the usual predict spectrum’s shape as soon as the number of particles decreases.PACS number(s):03.65.Fd (Algebraic methods),03.75.Fi (Bose condensation),42.50.Ct (Quantum statistical description of interaction of light and matter)The recent achievements of Bose–Einstein condensate(BEC)with a gas of atoms confined by a magnetic trap[1]has stimulated renewed interest in the question as to what signatures Bose–Einstein condensation imprints in the spectrum of light scattered from atoms in such a condensate[2,3].As well known,to deal with the dynamics of BEC gas the Bogolubov approxima-tion in quantum many-body theory[4]is an efficient approach,in which the creation and annihiliation operators for condensated atoms are substituted by c-numbers.One shortcoming of this method is that the total atomic particle-number may not be con-served after the approximation.Or a symmetry may be broken.To remedy this default,Gardiner[5]suggested a modified Bogolubov approximation by introducing phonon operators which conserve the total atomic particle number N and obey the bosonic commutation relation in the case of N→∞.In this sense,this phonon oper-ator approach gives an elegant infinite atomic particle-number approximation theory for BEC taking into account the conservation of the total atomic number.Along this line,the case offinite number of particle has been recentely investi-gated[6],and the algebraic method of treating the effects offinite particle number in the atomic BEC has been developed.It results a physical and natural realization of the quantum group theory[7]in the BEC systems,whose possibility was already suggested in[8],thought in a different manner.Here,we shall use the deformed algebra to study the response of a condensate withfinite number of atoms to the laser light and focus our attention on steady-state excitation.We consider a system of weakly interacting Bose gas in a trap and a classical radiationfield interacting with these two-level atoms,where b†,b denote the creation and annihiliation operators for the atoms in the excited state;a†,a,the creation and annihiliation operators for the atoms in the ground state.These operators satisfy theusual bosonic commutation relations.The Hamiltonian of the model readsH=¯h̟b†b+¯h g(t)b†a+g∗(t)ba† ,(1) where g(t)is a time-dependent coupling coefficient for the(classical)laserfield coupled to those two states with level difference¯h̟.Usually,the time dependence of g(t)is given by g exp(−iΩt),withΩbeing the frequency of the laser beam.Note that,with the above Hamiltonian,the total atomic particle number N= b†b+a†a is conserved.In the thermodynamic limit N→∞,the Bogolubov approxi-mation[4]is usually applied,in which the ladder operators a†,a of the ground state√are replaced by a c-numberN c g(t)b†+h.c.+ kΩk c†k c k+¯hN c−Γb(t)+√N c [3],whereγis the one-atom linewidth[9].Finally,b in(t)is the vacuum noise operatorb†in(t)b in(t′) = b in(t)b in(t′) =0,b in(t)b†in(t′) =δ(t−t′).(4)The solution of Eq.(3)is well known [9],and in the steady-state regime it becomesb (t ) ≡β=−ig √Γ+i ∆,(5)δb (ω)=√Γ+i ∆b in (ω),(6)where the semiclassical approximation b (t )=β+δb (t )has been used.In (6),δb (ω)is the Fourier component of the operator δb (t ).The spectrum of the light scattered from the atoms is given by the correlation of the operators b †(t )and b (t )[3].Hence,in the steady state,the spectrum of fluctuations δb †(ω)δb (ω′) results zero everywhere,by virtue of (6)and (4).This means that in the long time limit,only the equal time correlations survive.Let us now come back to the Bogolubov approximation [4].It destroyes the sym-metry of Hamiltonian (1),i.e.,the conservation of the total particle number is violated because [N,H ]=0.Then,to preserve the property of the initial model,it is possible to determine the following phonon operators [5]B =1N a †b ,B †=1N ab †.(7)These operators obey a deformed algebra [6].In fact,a straightforward calculation leads to the following commutation relationB,B † =1−2ηb †b ,(8)where we have introduced a small operator parameter η=1/N ,which for sufficientely large number of atoms is considered as c -number.The algebra defined by Eq.(8)belongs to the f -deformed algebra [10],where in general the deformed operator is related to the undeformed one through an operator valued function f asB =bf (b †b ).(9)In our particular case,we havef (b †b )=and for small deformation we getB≈b 1−ηN g(t)B†+h.c.+ kΩk c†k c k+¯h√Ng b†+b −¯h √2 b†b2+b†2b+ kΩk c†k c k+¯h√NgηN−Γb(t)+√NgηN−Γβ.(15)Of course,the solution of the above equation will be different from that of Eq.(5)(we refer to the latter asβ∞),but they approach each other as soon as N increases,as can be seen in Fig.1.The dynamics of the smallfluctuations is given by∂tδb(t)=Aδb(t)+Bδb†(t)+√Ngη(β+β∗),(17)B=i√Ξ(ω) [iω−A∗]b in(ω)+B b†in(ω) ,(19)whereΞ(ω)=|A|2−|B|2−ω2−iω(A+A∗).(20) Finally,the spectrum,by means of Eqs.(19),(20)and(4),readsS(ω)= dω′ δb†(ω)δb(ω′) =|B|2may lead(in the limiting case of small number of particles)to observable effects on a probe lightfield.Beyond the oversimplified model used,we retain the measurement of the light spectrum in presence of few condensed atoms a promising experimental challenge.On the other hand,the use of a BEC with small number of atoms would be the subject of next generation experiments[13].The same aim could be pursued in elementary particlefield as well.In fact,the BEC may also describe thefinal state of pions in high-energy-heavy-ion collisions[14,15].AcknowledgementsV.I.Man’ko is grateful to Russsian Foundation for Basic Research under the Project No.99-2-17753.References[1]M.H.Anderson J.R.Ensher,M.R.Matthews,C.E.Wieneman,E.A.Cornell,Science269,198(1995);K.B.Davies,M.-O.Mewes,M.R.Andrews.N.J.van Druten,D.S.Durfee,D.M.Kurn,W.Ketterle,Phys.Rev.Lett.75,3969(1995);C.C.Bradley,C.A.Sackett,J.J.Tollett and R.G.Hulet,Phys.Rev.Lett.75,1687(1995).[2]M.Levenstein and L.You,Phys.Rev.Lett.71,1339(1993);L.You,M.Lewensteinand J.Cooper,Phys.Rev.A50,R3565(1994);R.Graham and D.F.Walls,Phys.Rev.Lett.76,1774(1996).[3]J.Javanainen,Phys.Rev.Lett.72,2375(1994);75,1927(1995).[4]N.N.Bogolubov,J.Phys.(Moscow)2,23(1947).[5]C.W.Gardiner,Phys.Rev.A56,1414(1997).[6]C.P.Sun,S.Yu and Y.B.Gao,eprint qunt-ph/9809079.[7]L.C.Biedenharn,J.Phys.A22,L873(1989);A.J.Macfarlane,J.Phys.A22,4581(1989).[8]S.Mancini,V.I.Man’ko and P.Tombesi,Physica Scripta57,486(1998).[9]C.W.Gardiner,Quantum Noise(Springer,Heidelberg,1991).[10]V.I.Man’ko,G.Marmo,F.Zaccaria and E.C.G.Sudarshan,Physica Scripta55,528(1997).[11]S.Mancini,Physica Scripta59,195(1999).[12]B.R.Mollow,Phys.Rev.188,1969(1969).[13]G.M.Tino,private communication.[14]Proceedings of the Quark Matter’96Conference,(P.Braun-Munzinger et al.,eds.),Nucl.Phys.A610,1c-565c(1996);Proceedings of the Strangeness in Hadronic Matter’96Conference,(T.Csorgo et al.,eds.),Heavy Ion Physics4,1–440(1996).[15]T.Cs¨o rgo and J.Zimanyi,eprint hep-ph/9705432,eprint hep-ph/9705433.FIGURE CAPTIONSFig.1.A plot of the quantity||β|−|β∞||as a function of N.Values of the parameters are:∆=0and g=2.5γ.Furthermore,arg[β]=arg[β∞]=π/2∀N.Fig.2.The spectrum S as a function ofωand N.Values of parameters as in Fig.1.Nβοβο||||| − |501502503500.10.20.3240NFig.2 S. Mancini and V. I. Man'ko Spectrum of light scattered..........。

Light pack instruction 说明书

Light pack instruction 说明书

Fargo Pendants.INSTRUCTION MANUALThese products are only suitable for connection to a 240V~50Hz supply in accordance with current IEE wiring Regulations and should be installed in accordance with local Building Regulations andare for Domestic indoor ceiling use only and are not suitable for a Bathroom location.The light fitting should be connected to a lighting circuit protected by a 5 amp fuse (or a 6 amp miniature circuit breaker).If in doubt we recommend you contact a qualified electrician. Before installing your light fitting always:Switch off the mains supply and remove the appropriate fuse or switch off the appropriate circuit breaker before commencing installation.Ensure that no one else has access that would enable the supply to be inadvertently reconnected. Never fit bulbs of a higher wattage or of a type other than those specified on the label as this may cause overheating and damage the fitting.When fixing to the mounting surface ensure that the fixings used are appropriate for the mounting surface on which they are being used.The bulbs become hot during use so please switch off and allow 10 minutes to cool before replacing bulbs or cleaning the fitting.Clean with a dry cloth only. Do not use liquid or abrasive cleaners on this product.If any modification is made it will invalidate the warranty and may render the product unsafe.Before you startPlease read these instructions carefully before fitting your new light and retain for reference.Make sure that there are no pipes or cables beneath the mounting surface.Check the packaging and make sure that you have all the required parts.Follow each assembly step in order to prevent incorrect assembly.Make sure all screws / nuts, including electrical connections etc are fully tightened before use.This type of Light Fitting may be connected to a Dimmer if a Tungsten incandescent bulb is used. Ifa CFL type bulb is fitted then these cannot (generally) be controlled by a dimmer.These assembly diagrams are intended as a guide – if in doubt consult a qualified electrician.。

Jackson 吉他和贝斯手册说明书

Jackson 吉他和贝斯手册说明书

Congratulations! You’ve just joined countless others in what may be one of the best decisions you’ve ever made.For over 30 years , Jackson has been creating some of the finest guitars and basses in the music world. You are now the owner of one of them, so be proud. Long before the late, great Randy Rhoads walked into our shop, we made it our business to make the tools that musicians want. Take a few minutes to read this manual to become better acquainted with your new Jackson instrument. Understanding the correct setup procedure will keep your Jackson playing great in all conditions. Keep in mind that some procedures in this manual should only be performed by qualified technicians or persons who have experience in neck adjustments and intonation.JACKSON OWNER’S MANUAL ALL MODELS - GUITAR AND BASSCONTROLS1. VOLUME CONTROL: This knob acts as the master output of the guitar. Rotating the knob clockwise will increase the volume, counterclockwise will decrease the volume.2. TONE CONTROL: This knob acts as a high frequency roll off. With the knob turned fully clockwise, all frequencies are present. When the knob is turned counterclockwise, the higher frequencies are rolled off, giving a darker tone.3. PICKUP SELECTOR SWITCH: The pickup switch is used to switch between different combinations of the pickups. We use three main types of switches in most of our models. The 3-way slotted and toggle; the 5 way slotted ; and the Jackson JE-0005. The 3-way is used in most of our 2 pickup guitars and works as follows: 1=neck pickup; 2=neck and bridge pickup: 3=bridge pickup . The 5-way switch is used on many Jackson guitars in both 3-pickup and some 2-pickup models. In a 3-pickup model, the switch is as follows: 1=neck; 2=neck and middle; 3=middle; 4=middle and bridge; 5=bridge . The JE-0005 5-way switch operates as follows: 1=neck; 2=neck and bridge in parallel; 3=neck and bridge in series; 4=neck and bridge in parallel with filter; 5=bridge .BRIDGEJackson guitars use an assortment of bridge styles for various models. Here is a brief explanation of each type we use.1. Tune-o-matic: It has a simple height adjustment via two mounting posts. Intonation is adjusted by screws at each bridge saddle. The strings can either run through the body or attach to a stop bar tailpiece.2. Vintage Style Hardtail: String height is adjusted by small allen screws on each side of the saddles. Intonation is adjusted by the screws mounting the saddles to the rear of the bridgeplate.3. Vintage Style Tremolo: It is a very basic, 2 point fulcrum style tremolo with self centering saddles. This bridge is designed to rest flat on the body (non-floating).4. Vintage Style Floating Tremolo: This is an upgraded type of the Vintage Style tremolo. It can be adjusted to sit flat, or float above the body.5. Jackson Bass Bridge: We use a variety of low mass, high density, flat mounted bridges. On most of our Concert Basses, the bridges are convertible. This means the strings can be top loaded, or strung through the body. All have self centering saddles with individual intonation and string height adjustments.6. Double Locking Tremolos: This is the most common type of bridge, and can be found on most of our guitars. It is very simple to setup with a little guidance and patience. Note: For more information and technical tips and help,be sure to check out RESTRINGING THE DOUBLE LOCKING TREM1. Before loosening the strings, slip a small stack of business cards or a pencil under the bridge plate to maintain spring tension and keep the bridge parallel to the body.NOTE: There are many products on the market today that will assist in Floyd Rose® setups. Ask your localretailer for more info or check out our website .2. Loosen the 3 screws on the locking nut.3. Loosen all strings via the tuners on the headstock until there is no tension.4. Loosen the string clamping screws at bridge.5. Remove the strings from the guitar.6. Cut the ball end off the new strings.7. Insert the new strings between the clamping block and the saddle.8. Tighten the screws to lock the strings in place. Do not overtighten!9. Wind strings onto the tuners.10. Tune all stings to pitch, and stretch the strings by lightly pulling on them. Retune and repeat several times until thestrings will not detune.11. Repeat this process for all strings before tightening the locking nut and retuning using the fine tuners on the bridge.This is the one step that will determine the feel or “action” of your guitar. A few things should be taken into consideration before setting the intonation. What type, brand and gauge strings are you going to use? How high do you want the strings from the fretboard? How much spring tension do you want (how high do you want the bridge to float)? These will need to be determined before you get started. These steps should be completed in the order listed below.1. Neck Relief: The ideal neck setup will have a moderate amount of relief (curvature) to accommodate the vibrating strings. With the guitar tuned to pitch, fix a capo to the first fret, and depress the sixth string (low E) at the last fret. Measure the gap from the bottom of the string to the top of the 7th fret (using a feeler gauge, ruler with .010” increments, or similar tool) – the gap should be around .010” (see factory specs for more detail). If there is excessive relief, tighten the truss rod by turning it clockwise. If there is not enough relief, loosen the truss rod. Truss rod adjustments should be made in ¼ turn increments. The truss rod is located behind a plastic cover on the headstock of most Jackson instruments.2. Tremolo Spring Tension: This adjustment determines the neutral position of the tremolo. It is recommended to balance the spring tension with string tension – causing the bridge plate to sit parallel with the body. Heavier strings will require more spring tension, lighter strings (and drop tunings) will need less. To increase spring tension,tighten the 2 screws that hold the spring claw to the body (behind tremolo cavity cover on rear of body); loosen the screws to decrease tension.3. String Height: String height, or action, is measured as the distance between the bottom of the string and the top of the 17th fret (with strings tuned to pitch, no capo). If your tremolo or tune-o-matic bridge restson two mounting posts that go into the guitar body, the string height is adjusted by raising or lowering these posts. If your bridge is a vintage style or a bass, there are two allen wrench adjustments on each saddle that will raise and lower each string independently. Optimal string height depends on playing style and preference. See the factory specs section below for recommended string heights to get started. Low stringheight takes less effort to fret the strings, but may induce fret buzzing and less sustain if it’s too low.4. Pickup height: To set the pickup height, fret all strings at the last fret and use a 6” ruler (with 1/64” increments, or similar tool) to measure the distance from the bottom of the strings to the top of the pole pieces. The optimal distance depends on the type of pickup, and the player’s preference. See factory specs for pickup height guidelines.5. Intonation: All of the adjustments listed above must be completed prior to setting the intonation. Ensure that all strings are tuned to pitch. With intonation set properly, the 12th fret harmonic should be in tune with the 12th fret fretted note on every string. First play the 12th fret harmonic (lightly rest your finger on the string over the12th fret), and tune to pitch (use an electronic tuner for best results). Then, play the 12th fret fretted note (by evenly pressing the string on the 12th fret). If the fretted note is sharp, lengthen the string by moving the bridge saddle rearward. If flat, shorten the string by moving the bridge saddle forward. After adjusting the stringlength, retune the guitar (this will require unlocking the nut on guitars equipped with a double locking tremolo), andrepeat this procedure until the harmonic and fretted note are both in tune.FACTORY SPECSThe following are Jackson’s recommended neck relief, string height, pickup height, and string gauge specs. Please note that any problems that may arise from lowering the string height below our factory specifications, will not be covered by the Jackson warranty.NECK RELIEFGUITAR .007” - .008” (.18mm - .20mm)BASS.012” - .014” (.30mm - .36mm)STRING HEIGHTBASS SIDETREBLE SIDE GUITAR 4/64” (1.6mm)3/64” (1.2mm)BASS6/64” (2.4mm)5/64” (2.0mm)PICKUP HEIGHTBASS SIDETREBLE SIDE HUMBUCKER 4/64” (1.6mm)4/64” (1.6mm)STANDARD SINGLE COIL 5/64” (2mm)4/64” (1.6mm)NOISELESS SINGLE COIL8/64” (3.6mm)6/64” (2.4mm)FACTORY STRING GAUGES1st2nd 3rd 4th 5th 6th 7th 6 STRING GUITAR .009.011.016.024.032.042-7 STRING GUITAR w/ TREM.009.011.016.024.032.042.0527 STRING GUITAR w/o TREM.009.011.016.024.032.042.0544 STRING BASS .045,065.085.100---5 STRING BASS.045.065.085.100.125--GENERAL CAREThese are a few guidelines to keep your new Jackson in top form. The body, neck and headstock should be wiped clean with a clean soft cloth and a guitar polish after every use. The fingerboard should be cleaned every time you change strings. There are many cleaners on the market and most will dry the fingerboard (most window cleaning products have ammonia in them and will certainly dry the fingerboard dramatically) so be sure to oil the fingerboard after you clean it. There are many great oils today made just for fingerboards, so ask your local dealer for more information. Don’t let the board dry out, it will shrink and/or crack, causing the frets to raise up and become unlevel and unplayable. The hardware can be cleaned with a dry rag. If you have acidic perspiration or perspire excessively, please keep the hardware well oiled or it will rust and corrode. There are several tips on cleaning and maintaining your guitar on our website at .The Jackson you’ve chosen is a fine musical instrument and like any high quality product, care and regular maintenance should be a priority to help your guitar or bass last a lifetime. Thank you for choosing Jackson , we appreciate the opportunity to serve you. Please take a moment to fill out the enclosed owner’s registration and return it to us so that we may learn to better serve your needs. Also, be sure to read the care suggestions listedbelow. For more help be sure to visit our website at , thank you. For your own records, in case of loss, theft, etc., please fill in the following information and store it in a safe place.MODEL:__________________________________________________________________________COLOR:__________________________________________________________________________SERIAL NUMBER:_________________________________________________________________DEALER:________________________________________________________________________PURCHASE DATE:________________________________________________________________BATTERY REPLACEMENTOn all of our active circuits, 9 volt batteries are used to power-up. The systems feature the latest in IC circuitry, with very low power requirement. The battery is switched on when a cord is inserted into the input jack, so be sure to unplug the guitar/bass when not in use to avoid unnecessary power drain.NOTE: All PC1 guitars use an 18volt system (two 9 volt batteries) and both must be replaced as a pair in order for the sustainer system to function correctly. NOTE: Unless the instrument is equipped with a separate battery box, the battery is contained within the electric control cavity.CARE SUGGESTIONS~ NEVER store your guitar/bass in a hot car trunk! The HEAT WILL CAUSE SEVERE DAMAGE to your instrument.~ Always clean your strings after every use.~ Change strings at least every 20 playing hours.~ Wipe down the guitar with a clean, soft cloth after every use to remove sweat, etc from building up.~ Clean and oil fingerboard everytime you change strings.~ Do not overtighten any of the screws on the instrument. In most cases snug is best.~ When traveling by air be sure to detune strings by 1 step. Have an agent check your guitar before locking the case and tape the case closed to prevent tampering.~ Adjustments may need to be performed when you move your instrument into or out of different climates of altitude or humiditySTRING LOCK SCREWSINTONATION SCREWSSUSTAIN BLOCKGUITAR BODYBASE PLATEFINE TUNING SCREWS SADDLE。

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Instituto Superior T´ ecnico, Av. Rovisco Pais, P-1049-001 Lisboa, Portugal
Abstract
The spectra of light–light and heavy–light mesons are calculated within the framework of the QCD string model, which is derived from QCD in the Wilson loop approach. Special attention is payed to the proper string dynamics that allows us to reproduce the straight-line Regge trajectories with the inverse slope being 2πσ for light–light and twice as small for heavy–light mesons. We use the model of the rotating QCD string with quarks at the ends to calculate the masses of several light-light mesons lying on the lowest Regge trajectories and compare them with the experimental data as well as with the predictions of other models. The masses of several low-lying orbitally and radially excited heavy–light states in the D , Ds , B , and Bs meson spectra are calculated in the einbein (auxiliary) field approach, which has proven to be rather accurate in various calculations for relativistic systems. The results for the spectra are compared with the experimental and recent lattice data. It is demonstrated that an account of the proper string dynamics encoded in the so-called string correction to the interquark interaction leads to an extra negative contribution to the masses of orbitally excited states that resolves the problem of the identification of the D (2637) state recently claimed by the DELPHI Collaboration. For the heavy-light system we extract the constants
PACS:i
I. INTRODUCTION
The description of the mass spectrum of hadrons is one of the fundamental problems of strong interactions. It has been attacked in a sequence of approaches motivated by QCD, but still attracts considerable attention. One of the most intriguing phenomena — namely, the formation of an extended object, the QCD string, between the colour constituents inside hadrons, — plays a crucial role in understanding their properties. In the present paper this role is exemplified by spectra of the mass of light-light and heavy-light mesons. In the former case we study the role played by the QCD string in formation of the straight-line Regge trajectories and discuss the form of the interquark interaction inside light hadrons. For heavy-light mesons we find the masses of several low-lying states in the D , Ds , B , and Bs meson spectra including orbitally and radially excited ones. We calculate and discuss the spin-spin and spin-orbit splittings and compare them to experimental and recent lattice data. Special attention is payed to the role of the proper string dynamics in establishing the correct slope of the Regge trajectories for both light-light and heavy-light states, as opposed to those following from relativistic equations with local potentials. We remind the reader then that an extra piece of the effective interquark potential, the string correction, which is entirely due to the string-type interaction in QCD [1,2], gives a negative contribution to the masses of orbitally excited states. The latter observation allows us to resolve the “mystery” of an extremely narrow D (2637) state (and a similar one in the B -mesonic spectrum) [3] recently claimed by the DELPHI Collaboration [4,5]. We present a reasonable fit for the several lowest states in D - and B -mesonic spectra using the standard 2
values for the string tension, the strong coupling constant, and the current quark masses. We also find the correspondence between our model and Heavy Quark Effective Theory, extracting the constants used in the latter approach in the expansion of a heavy-light meson mass in the inverse powers of the heavy quark mass. We find analytical formulae for these constants and compare their numerical estimates with the predictions of other models. The two main approaches used in the numerical calculations are the quasiclassical method of solving the eigenenergies problem and the variational one based on the einbein field formalism. The accuracy of both methods is tested using exactly solvable equations and found to be about 7% at worst even for the lowest states. Possible improvements of the method are outlined and discussed. The paper is organized as follows. In Section II we give a brief insight into various aspects of the einbein field formalism. In Section III the exact spectra of relativistic equations are compared to the results of approximate calculations using the quasiclassical and variational einbein field methods, as well as the combined one. In Section IV we discuss the problem of the Regge trajectory slopes as they appear from the relativistic equations with local potentials and from the string-like picture of confinement. Derivation of the Hamiltonian for the spinless quark-antiquark system as well as of the spin-dependent corrections to it is the subject of Section V. The spectra of light-light and heavy-light mesonic states are calculated and discussed in Sections VI and VII, respectively. Section VIII contains our conclusions and outlook.
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