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簡介：南京航空航天大學(xué)碩士學(xué)位論文航空發(fā)動機(jī)CAT組態(tài)軟件技術(shù)研究姓名孫咪咪申請學(xué)位級別碩士專業(yè)航空宇航科學(xué)與技術(shù)（系統(tǒng)仿真與控制）指導(dǎo)教師張?zhí)旌?0091001航空發(fā)動機(jī)CAT組態(tài)軟件技術(shù)研究IIABSTRACTTHECOMPUTERAIDEDTESTCATTECHNOLOGYHASBEENPREVAILEDINTHEAEROENGINETESTFIELDITISCONSIDEREDUNDESIRABLEUSINGTHECOMMERCIALCONFIGURATIONSOFTWAREASTOOLSTODEVELOPTHECATSOFTWAREBECAUSEOFTHEINFEASIBILITYOFGENERATINGSOURCECODESCOMPLEXITYOFPRECEDINGTHESECONDARYDEVELOPMENTITISTHOUGHTASAHUGEMISSIONTOESTABLISHCATSOFTWAREBASEDONTHEVISUALCENVIRONMENTSTARTINGFROMTHECODINGPERIODTHELOWEFFICIENCYOFDEVELOPINGWKISUNACCEPTABLETHEREFEITISNECESSARYTODEVELOPASTOFRAPIDEFFECTIVEMETHODFAEROENGINEIENTEDTESTWHICHISOPENSOURCEACCELERATESTHECATSOFTWAREDEVELOPPERIODTHISPAPERSTSONTHEPOINTOFHALFCUSTOMIZEDPHILOSOPHYFSTUDYINGTHEAEROENGINECATCONFIGURATIONSOFTWARETECHNOLOGYTHEAEROENGINETESTCATSOFTWARECONFIGURATIONDEVELOPMENTPLATFMCATCDPWASDEVELOPEDINVISUALCENVIRONMENTITMAINLYCONTAINSCONFIGURATIONPROGRAMDEVELOPMENTTEMPLATEPROGRAMDEVELOPMENTCODEAUTOGENERATIONPROGRAMDEVELOPMENTTHECONFIGURATIONPROGRAMISINGEOFCOLLOCATINGUSERREQUIREDFUNCTIONALMODULESSAVINGTHECONFIGURATIONINFMATIONTHEUSERFRIENDLYCONFIGURABLEENVIRONMENTWASDESIGNEDTHECONFIGURABLEDATABASEPARAMETERFUNCTIONWASREALIZEDWITHTHEHELPOFDAODATABASEACCESSTECHNOLOGYTHETEMPLATEPROGRAMISEMPLOYEDFDATAACQUISITIONPARAMETERILLUSTRATIONSERIALPTCOMMUNICATIONETCWHICHISTHECNERSTONEOFTHECATARCHITECTUREONTHEBASISOFANALYZINGTHEFEATURESOFCATSOFTWARETYPICALFUNCTIONSTHECRESPONDINGUSERINTERFACEUIWEREDESIGNEDTHEYWERECLASSIFIEDSAVEDINTOTHETEMPLATEFOLDERTOBETREATEDASTHESOURCEOFTHECODEAUTOGENERATIONPROGRAMTHECODEAUTOGENERATIONPROGRAMISUSEDTOPRODUCETHEUSERCUSTOMIZEDCATARCHITECTUREPROGRAMWHICHISNATUREDFTHEMANAGEMENTOFCOPYINGTHETEMPLATECODESACCDINGTOTHECONFIGURATIONINFMATIONAHIERARCHALDESIGNINGMETHODWASBROUGHTFWARDSTODESIGNTHECODEAUTOGENERATIONPROGRAMACERTAINVECTNOZZLECATPROGRAMAMICROTURBOJETENGINECATPROGRAMWEREDEVELOPEDWITHCATCDPITWASPROVEDTHATCATCDPSIGNIFICANTLYENHANCEDTHEEFFICIENCYOFCATSOFTWAREDEVELOPMENTTHECATSOFTWAREDEVELOPMENTWITHCATCDPCOULDMEETTHESPECIFICATIONOFAEROENGINETESTKEYWDSAEROENGINECATCOMPUTERAIDEDTESTCONFIGURATIONSOFTWARECATCDPCATSOFTWARECONFIGURATIONDEVELOPMENTPLATFMCODEAUTOGENERATION

簡介：分類號密級學(xué)校代碼學(xué)號西北工業(yè)大學(xué)碩士學(xué)位論文Y85713810699036104107題目基塹窒塞塑扭遇撿盤查士苧鮑堡廛盆塹當(dāng)查金鹽簋作者盟蛐指導(dǎo)教師至三氐專業(yè)技術(shù)職務(wù)塾筮學(xué)科專業(yè)墊拭遮鹽壟堡逾答辯日期2QQ魚13學(xué)位授予日期西北上業(yè)大學(xué)碩士學(xué)位論文ABSTRACTABSTRACTTHETURBINEDISCANDBLADEWHICHARETHEKEYCOMPONENTOFENGINETUBINEROTORSYSTEMWORKUNDERABOMINABLECONDIATIONOFHIGHCYCLICTEMPERATUREANDMECHANICALLOADINORDERTOENSURETHESTABILITYANDRELIABILITYOFTHEAIRPLANEWHENITISINSERVICEANACCURATEANALYSISOFTHESTRENGTHANDTHEFATIGUELIFEFORTHETURBINEDISCANDBLADEARENEEDEDIMMINENTLYTILISPAPERSTUDIESASATISFYINGRESULTOFTHESTRENGTHANDLIFEPREDICATIONUNDERTHEBACKGROUNDOFNEEDINGTOPROLONGACIVILAVIATIONTURBINELIFEFIRSTLYTHISPAPERSUMMARIZESTHEDISPOSALOFTHEFLIG1TMISSIONPROFILE，ANDFOCUSESONNINETEENACTUALFLIGHTCYCLICLOADDATA，THERAINFLOWCOUNTLOADINGCYCLESANDLOADINGDURATIONOFTHEROTATESPEEDANDEXHAUSTTEMPERATUREETCISOBTAINEDBYSTATISTICALCALCULATIONANDTHEDAMAGEOFTHEPARTIALLOADINGCYCLESISANALYZEDBASEDONTHEANALYSISABOVE，WEWIPEOFFTHEINVALIDLOADDATAWHICHDONOHARMONTHEFATIGUEDAMAGEANDANACTUALCYCLICLOADSPECTRUMISOBTAINEDTHISLOADSPECTRUMWHICHISTHEGROUNDWORKFORTHESTRENGTHAND1IFEOFTHETURBINEROTORSYSTEMPROVIDESTHEBASISOFFORMULATINGACCELERATEDMISSIONTESTSPECTRUMSECONDLYANSYSSOFTWAREISEMPLOYEDTOCONSTRUCTATHREEDIMENSIONALFINITEELEMENTMODALOFTURBINEDISCANDBLADECIRCUMSTANCESOFTHECONTACTNONLINEARBETWEENTUBINEDISCMORTISEANDBLADETENONTHEELASTICPLASTICITYDEFORMATIONOFMATEDALANDTHETHERMALSTRESSCAUSEDBYNONUNIFORMTEMPERATUREARECONSIDEREDANDATHREEDIMENSIONNONLINEARCYCLICSTRESSSTRAINANALYSISISCONDUCTEDTHEN，THEDANGEROUSPOINTCAUSEDBYFATIGUERUPTUREISFOUND，THESTRESSPROFILEISESTABLISHEDFURTHERMORE，THESTATICSTRENGTHOFTHETURBINEDISCANDBLADEISSTUDIEDBYUSINGEGD一3RULEFINALLYDEPENDONTHESTRESSSTRAINANALYSISRESULTSANDTHEMATERIAL’SFATIGUECHARACTERISTICSWESELECTSNCURVEMETHODANDMANSONCOFLIRTFORMULARESPECTIVELYFORTHEFATIGUEDAMAGECALCULATIONANDLIFEPREDICTIONOFTHETURBINEDISCBYUSINGTWODIFFERENTLIFECALCULATIONMETHODSWHICHAREMENTIONEDABOVCTHESAMERESULTISDERIVEDTODEMONSTRATETHEVALIDITYANDEFFICIENCYOFTHEMETHODANDCALCULATIONPROCESSWEFINDTHETURBINEBLADEISONTHECOMPLICATEDSTRESSSTATUSSOFODRDIFFERENTRULESFORACHIEVINGEQUIVALENTSTRESSAREUSEDTOCONTRASTTHENTHEFATIGUELIREOFTHETUBINEBLADEISACHIEVEDBYUSINGLARSONMILLERFORMULATHROUGHTHEANALYSISOFSTRESSANDLIFEABOVETHISPAPERPROVIDESAREFERENCETOIMPROVINGTHERELIABILITYANDPROLONGINGTHEFATIGUELIFEOFTHETUBINEKEYWORDLOADSPECTRUM，TUBINEDISC，TUBINEBLADE，STRENGTH，F(xiàn)ATIGUEDAMAGE，1IRECALCULATIONII

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簡介：南京航空航天大學(xué)博士學(xué)位論文航空多框整體結(jié)構(gòu)件銑削變形機(jī)理與預(yù)測分析研究姓名郭魂申請學(xué)位級別博士專業(yè)機(jī)械制造及其自動化指導(dǎo)教師左敦穩(wěn)20051201航空多框整體結(jié)構(gòu)件銑削變形機(jī)理與預(yù)測分析研究IIABSTRACTITISVERYDIFFICULTTOPREDICTTHECNCMACHININGDISTORTIONOFMONOLITHICMULTIFRAMECOMPONENTSINAEROINDUSTRYBYEITHERTHEORETICALANALYSISOREXPERIMENTALRESEARCH,BECAUSEOFTHEIRCOMPLICATEDSTRUCTURETHEMACHININGDISTORTIONBECOMESONEOFTHENECKPROBLEMSINTHERAPIDDEVELOPMENTANDTHEEFFECIENTPRODUCTINOFOURNATIONALDEFENSEWEAPONSBYUSINGFINITEELEMENTSIMULATIONANDEXPERIMENTS,ADEEPSTUDYISCARRIEDOUTONTHEMECHANISM,THEPREDICTIONMETHODANDTHEVARIATIONTENDENCYOFTHEMILLINGDISTORTIONTHEWORKINTHISDISSERTATIONCANPROVIDEABASISFORTHEDISTORTIONCONTROLOFTHEMONOLITHICMULTIFRAMECOMPONENTSSEVENCHAPTERSAREINCLUDEDINTHISDISSERTATION,ANDTHEMAINWORKISASFOLLOWSINCHAPTER1,THEBACKGROUNDANDSIGNIFICANCEOFTHISRESEARCHISINTRODUCEDFIRSTLYTHEN,THESTATEOFTHEARTINTHERESEARCHOFMACHININGDISTORTIONOFTHEMONOLITHICCOMPONENTISSUMMARIZEDFINALLY,THEMAINCONTENTSANDFRAMESTRUCTUREOFTHISDISSERTATIONARESHOWNINCHAPTER2,BASEDONTHESTATUSANALYSISONTHERESEARCHOFMILLINGFORCE,ITSCHARACTERISTICISSTUDIEDFORTHEAEROMATERIALOFALUMINUMALLOY7075T7351,ANDTHEEMPIRICALMODELISESTABLISHEDBYUSINGTHEREGRESSIONORTHOGONALEXPERIMENTALMETHODWHERETHEFACTORNUMBERISFIVEANDTHESTANDARDNUMBERISFOURTHEREFORE,ABASEISPROVIDEDFORSTUDYINGTHEEFFECTOFMILLINGFORCEONTHEMACHININGDISTORTIONINCHAPTER3,ACCORDINGTOTHEMILLINGCHARACTERISTICSOFTHEMONOLITHICMULTIFRAMECOMPONENTS,THEMECHANICSBASISISDISCUSSEDAFTERTHAT,MECHANICALDESCRIPTIONANDTHE3DMODELINGRULESAREGIVEN,ANDTHEFINITEELEMENTMODELOFTHEMILLINGDISTORTIONOFTHEMULTIFRAMECOMPONENTSISESTABLISHEDFINALLY,THETECHNICROUTEFORTHERESEARCHOFMILLINGDISTORTIONISPROPOSEDINCHAPTER4,THEEFFECTOFTOOLPATHANDCLAMPINGSCHEMESONRESIDUALSTRESSESASWELLASMACHININGDISTORTIONAREANALYZEDBYUSINGTHREEDIMENSIONALELASTICPLASTICFEMFINITEELEMENTMETHODTHEDISTORTIONVARIATIONTENDENCYUNDERFOURTYPICALTOOLPATHS,THEPRESSINGPLATECLAMPINGANDSTRETCHEDFIXATIONISOBTAINEDRESPECTIVELY

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簡介：中圖分類號TM461論文編號102870316SZ020學(xué)科分類號085207碩士學(xué)位論文航空三相橋式PWM整流器開關(guān)管故障診斷與容錯控制技術(shù)研究研究生姓名許政專業(yè)類別工程碩士專業(yè)領(lǐng)域電氣工程指導(dǎo)教師肖嵐教授南京航空航天大學(xué)研究生院自動化學(xué)院二О一六年三月NANJINGUNIVERSITYOFAERONAUTICSANDASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFAUTOMATIONENGINEERINGRESEARCHONDIAGNOSISANDFAULTTOLERANTCONTROLTECHNOLOGYOFSWITCHONTHREEPHASEBRIDGEPWMRECTIFIERFORAIRCRAFTAPPLICATIONATHESISINELECTRICALENGINEERINGBYXUZHENGADVISEDBYPROFESSORXIAOLANSUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFORTHEDEGREEOFMASTEROFENGINEERINGMARCH,2016

簡介：中圖分類號V2337論文編號102870216SZ015學(xué)科分類號085232碩士學(xué)位論文面向航空電動燃油泵的齒輪泵研究研究生姓名錢一凡專業(yè)類別工程碩士專業(yè)領(lǐng)域航空工程指導(dǎo)教師葉志鋒教授南京航空航天大學(xué)研究生院能源與動力學(xué)院二О一六年三月NANJINGUNIVERSITYOFAERONAUTICSASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFENERGYPOWERENGINEERINGRESEARCHONGEARPUMPFAVIATIONELECTRICFUELPUMPATHESISINAERONAUTICALENGINEERINGBYQIANYIFANADVISEDBYPROFYEZHIFENGSUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFTHEDEGREEOFMASTEROFENGINEERINGMARCH2016

簡介：貴州大學(xué)碩士研究生畢業(yè)論文分類號密級論文編號貴州大學(xué)2012屆碩士研究生學(xué)位論文偏心及共振對航空高速電機(jī)軸的疲勞研究學(xué)科專業(yè)機(jī)械制造及自動化研究方向現(xiàn)代先進(jìn)設(shè)備制造導(dǎo)師張衛(wèi)研究生劉剛中國﹒貴州﹒貴陽2015年3月貴州大學(xué)碩士研究生畢業(yè)論文I偏心及共振對航空高速電機(jī)軸的疲勞研究摘要在現(xiàn)代軸類零件疲勞壽命研究中，由于安裝誤差而引起兩軸承之間不對稱產(chǎn)生偏角的研究已經(jīng)有很多且很成熟，但是由于振動以及安裝誤差而引起軸端的偏心對軸的疲勞壽命研究分析很少，且針對偏心及振動提出一個普遍實用的解決方法也很少。所以對軸類零件進(jìn)行共振驗證以及軸端偏心對疲勞壽命的影響研究具有十分重要的意義。本文通過對斷軸斷面形貌斷裂紋理分析，得到了此軸類零件斷裂主要是由于偏心、振動、斷口端面在旋轉(zhuǎn)的同時承受彎矩共同作用，斷裂性質(zhì)均為扭矩剪切應(yīng)力作用下形成的過載斷裂。對電機(jī)轉(zhuǎn)子進(jìn)行轉(zhuǎn)子動力學(xué)分析，得到了轉(zhuǎn)子的三階臨界轉(zhuǎn)速15655RMIN，22558RMIN，22765RMIN，與電機(jī)轉(zhuǎn)速11076RMIN對比，接近轉(zhuǎn)速安全裕度分別為858和509，均大于危險裕度10，研究說明了電機(jī)轉(zhuǎn)子不會因為臨界轉(zhuǎn)速與額定轉(zhuǎn)速接近而發(fā)生共振影響軸的疲勞壽命，同時通過模態(tài)仿真分析與固有頻率試驗分析驗證了仿真與試驗數(shù)據(jù)的準(zhǔn)確性同時也說明了電機(jī)不會因為固有頻率而引起共振對軸疲勞壽命產(chǎn)生影響。對軸伸端進(jìn)行實際偏心及應(yīng)力理論計算，實際極限偏心為0125MM，軸上薄弱處應(yīng)力值大小為78544MPA，通過ANSYS有限元仿真分析軟件對航空電機(jī)主軸進(jìn)行模擬工況邊界條件應(yīng)力分析得到軸上薄弱處應(yīng)力大小為752MPA，驗證了計算結(jié)果與仿真分析的準(zhǔn)確性，為主軸應(yīng)力設(shè)計提供了可參考依據(jù)。查閱航空材料手冊得到了30CRMNSI材料的疲勞壽命曲線，并求得了曲線上13個應(yīng)力點對應(yīng)的疲勞壽命循環(huán)次數(shù)，根據(jù)斷軸處應(yīng)力大小和SN曲線擬合得到斷軸處的疲勞壽命為20674個周期。針對在偏心及振動對軸類零件疲勞壽命的影響，提出了軸承在預(yù)緊力下及在軸承與襯套之間添加橡膠墊圈起到減振及偏心固定端轉(zhuǎn)移的目的使軸類零件壽命得到了大大的提高，并且通過每200H記錄電機(jī)前端、后端、后端側(cè)面振動的方法對電機(jī)進(jìn)行了1500H的壽命實驗，且電機(jī)各部件仍能正常工作。通過理論有限元仿真讓改善前后軸上薄弱處應(yīng)力對比，未加橡膠圈時軸上薄弱處應(yīng)力為78544MPA，加了橡膠圈后軸上薄弱處應(yīng)力大小為9578MPA，說明在相同極限偏心0125MM下，軸承與襯套接觸面開槽加橡膠圈的方法使軸上薄弱處應(yīng)力大大的減小。為今后軸類零件提高疲勞壽命的實際運用方法研究提供了可參考的理論依據(jù)。關(guān)鍵字偏心；共振；理論驗證；有限元仿真；疲勞壽命

簡介：天津大學(xué)碩士學(xué)位論文民航空管網(wǎng)絡(luò)與信息安全管理體系的構(gòu)建研究姓名李大海申請學(xué)位級別碩士專業(yè)管理科學(xué)與工程指導(dǎo)教師陳通20090801ABSTRACTAIRTRAFFICCONTROLLARGESCALEINFORMATIONSYSTEMS，INVOLVINGTHEAPPLICATIONOFMANYBUSINESSRELYINGONAHIGHDEGREEOFSECURITYTHROUGHTHECONSTRUCTIONOFAIRTRAMCCONTROLTOPROTECTINFORMATIONRESOURCESARENOTVIOLATEDTOENSURETHATINFORMATIONRESOURCESAREMINIMALRISKSANDMAXIMIZETHESECURITYBENEFITS，TOENSURET11ATTHEATCINFORMATIONINFRASTRUCTUREINFORMATIONSERVICESANDSUPPORTFACILITIESWITHTHECONFIDENTIALITYINTEGRITYAVAILABILITYCONTROLANDIMPROVEAIRTRAFFICCONTROLTHELEVELOFINFORMATIONSECURITYTHEPROTECTIONOFNATIONALSECURITYSOCIALSTABILITYANDECONOMICDEVELOPMENTTHEREFORE。INORDERTOEFFECTIVELYPREVENTANDRESOLVEINFORMATIONSECURITYRISKS，TONATIONALLEVELINFORMATIONSYSTEMSECURITYREQUIREMENTSTOPROTECTANDENSURETHESMOOTHOPERATIONOFINFORMATIONSYSTEMSANDOPERATIONSONGOING，AVIATIONSECURITYFORTHEPEOPLEESCORTINGTUBEISNECESSARYTOESTABLISHEFFECTIVEINFORMATIONSECURITYSYSTEM，ANDENHANCEINFORMATIONSECURITYANDAIRTRAFFICCONTROLCAPACITYTOGUARDAGAINSTRISKSTHISPAPERONTHEISSUEOFAIRTRAFFICCONTROLINFORMATIONSECURITYMANAGEMENTONTHECONSTRUCTIONOFSOSHALLOWINTHISPAPERTHEMAINCOMPONENTSFROMTHEFIVECHAPTERSTHEFIRSTCHAPTERISTHEINTRODUCTION，ANALYSISOFTHEIMPLEMENTATIONOFAIRTRAFFICCONTROLNETWORKANDINFORMATIONSECURITYSYSTEMOFTHENEEDTOSTUDYAIRTRAMCCONTROLNETWORKANDINFORMATIONSECURITYOBJECTIVESANDTHESIGNIFICANCEOFTHERESEARCHCONTENTINTHISARTICLESTRUCTURE，ANDINSU伍CIENT；CHAPTERIIINTRODUCEDTHENETWORKANDINFORMATIONSECURITYRELATEDCONCEPTSANDTHEMAINTHEORYANDPUBLICCONTROLOFINFORMATIONSECURITYAVIATIONLAWSANDREGULATIONS；CHAPTERIUFOCUSESONTHENETWORKANDINFORMATIONSECURITYINTHEPROCESSOFHISTORICALEVOHTIONTLLEDEVELOPMENTOFNETWORKANDINFORMATIONSECURITYTHEAIRMANAGEMENTINFORMATIONSYSTEMSECURITYPROBLEMSANDCAUSEANALYSIS；THEFOURTHCHAPTERINTRODUCESTHECHARACTERISTICSOFAIRTRAMCCONTROLINSHENZHENNETWORKANALYSISSHERTZHENATCNETWORKANDINFORMATIONSECURITYPROBLEMSANDCOUNTERMEASURESINPRACTICEASWELLASAIRTRAFFICCONTROLNETWORKTOPOLOGYSHENZHENMAJORPRACTICEMANAGEMENT；THEFI鈾C(jī)HAPTERTOIMPROVEAIRTRAFFICCONTROLNETWORKANDINFORMATIONSECURITYSYSTEMOFIDEASTOBUILDANDIMPROVETHEAIR訂A伍CCONTROLNETWORKANDINFORMATIONSECURITYSYSTEMTOBUILDPRINCIPLESANDMETHODS，ANDANALYSISOFRESISTANCETHATMAYBEENCOUNTEREDANDSOLUTIONSKEYWORDSAVIATIONATC；NETWORK；INFORMATION；SAFETY；MANAGEMENTSYSTEM；CONSTRUCTIONSTUDY

簡介：中圖分類號V2319論文編號102870216S073學(xué)科分類號082502碩士學(xué)位論文航空發(fā)動機(jī)轉(zhuǎn)子系統(tǒng)的參數(shù)化設(shè)計及組合優(yōu)化方法研究研究生姓名付堯?qū)W科、專業(yè)航空宇航推進(jìn)理論與工程研究方向結(jié)構(gòu)強(qiáng)度與完整性指導(dǎo)教師羅貴火副教授南京航空航天大學(xué)研究生院能源與動力學(xué)院二О一六年三月承諾書本人聲明所呈交的碩士學(xué)位論文是本人在導(dǎo)師指導(dǎo)下進(jìn)行的研究工作及取得的研究成果。除了文中特別加以標(biāo)注和致謝的地方外，論文中不包含其他人已經(jīng)發(fā)表或撰寫過的研究成果，也不包含為獲得南京航空航天大學(xué)或其他教育機(jī)構(gòu)的學(xué)位或證書而使用過的材料。本人授權(quán)南京航空航天大學(xué)可以將學(xué)位論文的全部或部分內(nèi)容編入有關(guān)數(shù)據(jù)庫進(jìn)行檢索，可以采用影印、縮印或掃描等復(fù)制手段保存、匯編學(xué)位論文。（保密的學(xué)位論文在解密后適用本承諾書）作者簽名日期

簡介：分類號密綴單位代碼學(xué)號罾牡；蓑蟲唾。10699046076395碩士學(xué)位論文學(xué)位研究生作者趙瑾指導(dǎo)教師趔握迭專業(yè)技術(shù)職務(wù)夔授申請學(xué)位日期2007．3西北工業(yè)大學(xué)碩士學(xué)位論文ABSTI己ACTPRACTICC蛐GPLAYSAVERYIMPONA呲ROLEILLCOMPREHENDIILGANDM船TERING幽RYKILOWLEDGES，HOWEVER，ITCAN’TSATIS句STLLDENTS’PI枷CEREQMREMEM鋤DIIIⅦ，ROVETE∞HINGQULITYBE戤M∞OFOUT0FDALEINS仃ILCTI伽IALIN蛐MM蜘L協(xié)觚DEXPEILSIVEEXPE曲鼬TFHNDINAIRCRARMAJOTWITHTHEDEVELOPMENTOFCOMPUTER，VINI瑤LREALI鑼ISTOBEUSEDWIDELYINEDUCATIONREGION．、_RJNLIALRCALI哆T啪S2DTE∽HING鍘【VIRO姍ENT硒INT啪DIVE鋤DREAIISDC3DTEACLLINGENVIRONMENT，SOTLLAL“COMRIBUTESTHCSTLLDY枷VATION托DKMDSONCAP∞ITYOFSTUDEN協(xié)．THEINVESTIGATEDSLL_巧ECTPRESENTEDHEREIILFOC嵋ESPRIMADLYONTE觚城NG觚DC【P蔭M∞T，ANDSCENESIMLLLATIONSYSTEMOFAEROEN垂NETCACLLINGEXPE吐MEMSARESETLLP．PANICLLL盯柚ALYSESOFTHISSYSTEINARECOMPLCTLED自DMTHE咖TIL托鋤DAEFODYLL鼬ICD眥ACTERISTIC，SOTLLATTLLREEDIMENSI伽IAL、，IRUTAIAEFO．EI瑪INELA．BORATORYCOLLLDBEBLLIK觚DMANYEXPERIM∞TSTEACLLING嘶LLBCPERF．O徹ED，SIICH嬲，THC刪鵲SEMLLYOFEN西北，THEEXPERIMEMSIMLLLATIONOFTCSTBAY，THESIINILLATIILGOFENGILLEWORKIILG肌DMCEXPTRINLENTSILLLMA矗ONOFNOWFIELD，ETC．NEABILITYOFS黜SIN】LMATI∞IN也E掰O鋤酉∞EXPE血N％TALLABORA衄YISCARRICDOMBYMETBR∞D(zhuǎn)IINENSIONDYNAIILICMODELBUILDING觚DSCENES砌ATIONDFIV％Ⅵ恤CHISMECO∞由。D1ILIQ∞OFSCENESIMUL撕ONBASED∞MLILTIG％CRCATOR，VBGA；THEIMEMCTIVEF．啪CTIONWHICHCOMPLN．MGDESCERPTION孤D船SCMBLAGEOFAEROENGINEMODELISPERF．O肌EDBYTHEVI刪HAILDB雒EDONME脅西OVES姐DCOUISIONDET∞矗OIL，SHOWIILGTLLESMMGCHARACTERIS6CONTHEIM口邳TIONOFVIRTILALRCALITY；THCPRILLCIPLEOFTHESTE∞∞“SI∞IS細(xì)的DUCED鋤DTL尬LARGCSC他∞ADOPTINGTHEPOLARI刎ONISPUTF0，捌，WMCHSUPPLYTHELLARD眥PLATFO咖FORTHEVISUALH姍ERSIONOFME、，JNL】ALREAL時；齜PRILLCIPLEOFST啪L婦SGCNCRATIONIS姐ALYZED，ME、，ISLLALMEMODFORNLCP枷HOFTHENUIDMATERIALP枷CAL璐ING也ELINEEL鋤∞TMETHODISP把辯MED．THEPAPERDEVELOPSSUCCESSMISIIILULATIONSYSTEMFORTLLEI船TNLCDONALLAT唧MTORYSYSTEMONTHE舢一ELLGINE，BASCDONTLLED鋤ONSTRATIONDETAILEDILL眥INATEDABOVCAND讎塒NCIPL∞OFTHE∞ROEN西NE，嬲WCLL髂MEFI渤GTESTDATA．II

簡介：國內(nèi)圖書分類號TG54國際圖書分類號621西南交通大學(xué)研究生學(xué)位論文密級公開年級2Q壘級姓專二零一七年五月一零一屯牛血月的一撾材一金窒復(fù)盟題術(shù)一壓一技一星量綞加一紅削一碳一銑一用一空一工匹E目阻一西南交通大學(xué)學(xué)位論文版權(quán)使用授權(quán)書本學(xué)位論文作者完全了解學(xué)校有關(guān)保留、使用學(xué)位論文的規(guī)定，同意學(xué)校保留并向國家有關(guān)部門或機(jī)構(gòu)送交論文的復(fù)印件和電子版，允許論文被查閱和借閱。本人授權(quán)西南交通大學(xué)可以將本論文的全部或部分內(nèi)容編入有關(guān)數(shù)據(jù)庫進(jìn)行檢索，可以采用影印、縮印或掃描等復(fù)印手段保存和匯編本學(xué)位論文。本學(xué)位論文屬于1保密口，在年解密后適用本授權(quán)書；2不保密函使用本授權(quán)書。請在以上方框內(nèi)打“寸’學(xué)位論文作者虢加修陬日期州7羅2L指導(dǎo)老師簽名二丁【日期PF7，礦