簡介：南京理工大學(xué)碩士學(xué)位論文民航華北地區(qū)飛行計劃一體化處理系統(tǒng)的設(shè)計與實現(xiàn)摘要飛行計劃的一體化處理就是實現(xiàn)飛行計劃的統(tǒng)一申請、統(tǒng)一生成、統(tǒng)一更新和統(tǒng)一發(fā)布，解決目前飛行計劃由各管制中心單獨管理而造成的一致性和完整性問題，為區(qū)域提供準(zhǔn)確一致的飛行計劃數(shù)據(jù)服務(wù)。飛行計劃一體化處理是對現(xiàn)有民航飛行計劃管理模式的一次革命性改進，對建設(shè)我國民航高效的空中交通服務(wù)體系具有重要意義。飛行計劃一體化處理在國外已有成功應(yīng)用的先例，中國民航正對飛行計劃一體化處理進行技術(shù)論證。民航華北空管局依據(jù)對飛行計劃一體化的理解，結(jié)合自身飛行計劃管理的特點，提出了區(qū)域飛行計劃一體化處理的需求，并與中國電子科技集團公司第二十J、研究所合作進行民航華北地區(qū)飛行計劃一體化處理系統(tǒng)設(shè)計開發(fā)。本文結(jié)合民航華北地區(qū)飛行計劃一體化處理系統(tǒng)的系統(tǒng)研制過程，重點論述了經(jīng)用戶確認(rèn)的系統(tǒng)設(shè)計及實現(xiàn)方案，并對系統(tǒng)的關(guān)鍵技術(shù)和系統(tǒng)結(jié)論進行了論述。關(guān)鍵詞飛行計劃空中交通管理一體化AFRN流量管理聲明本學(xué)位論文是我在導(dǎo)師的指導(dǎo)下取得的研究成果，盡我所知，在本學(xué)位論文中，除了加以標(biāo)注和致謝的部分外，不包含其他人已經(jīng)發(fā)表或公布過的研究成果，也不包含我為獲得任何教育機構(gòu)的學(xué)位或?qū)W歷而使用過的材料。與我一同工作的同事對本學(xué)位論文做出的貢獻均己在論文中作了明確的說明。研介“洲率一如石年‘，月歲。日學(xué)位論文使用授權(quán)聲明南京理工大學(xué)有權(quán)保存本學(xué)位論文的電子和紙質(zhì)文檔，可以借閱或上網(wǎng)公布本學(xué)位論文的全部或部分內(nèi)容，可以向有關(guān)部門或機構(gòu)送交并授權(quán)其保存、借閱或上網(wǎng)公布本學(xué)位論文的全部或部分內(nèi)容。對于保密論文，按保密的有關(guān)規(guī)定和程序處理。研究、一墊Q車J。若年，，月了。日

簡介：南京航空航天大學(xué)碩士學(xué)位論文小型太陽能飛機氣動結(jié)構(gòu)推進一體化設(shè)計研究姓名鄧海強申請學(xué)位級別碩士專業(yè)飛行器設(shè)計指導(dǎo)教師余雄慶20061201小型太陽能飛機氣動結(jié)構(gòu)推進一體化設(shè)計研究IIABSTRACTSOLARPOWEREDAIRCRAFTISANELECTRICPOWEREDAIRCRAFTWHICHTAKESPOWERFROMSOLARRADIATIONITISTHEOUTCOMECOMBININGAERONAUTICALTECHNOLOGYWITHNEWENERGYTECHNOLOGYASANEWCONCEPTOFAIRCRAFTITSAERODYNAMICSTRUCTURALPROPULSIVESYSTEMSAREDEEPLYCOUPLEDTHISTHESISAIMSATHOWTOAPPLYMULTIDISCIPLINARYDESIGNOPTIMIZATIONMETHODSTOTHEINTEGRATEDAERODYNAMICSTRUCTURALPROPULSIVEDESIGNOFTHESOLARPOWEREDAIRCRAFTBASEDONTHETWOLEVELOPTIMIZATIONAPPROACHWEDECOMPOSEDTHEINTEGRATEDDESIGNINTOASYSTEMLEVELOPTIMIZATIONTHREESUBSYSTEMLEVELOPTIMIZATIONSTHETASKOFSYSTEMLEVELOPTIMIZATIONISTOFINDTHESHAREDAUXILIARYDESIGNVARIABLESTOMINIMIZETHETAKEOFFWEIGHTSUBJECTTOTHECONSISTENCYCONSTRAINTSTHETASKOFEACHSUBSYSTEMOPTIMIZATIONISTOFINDTHELOCALDESIGNVARIABLESTOMINIMIZEMAXIMIZEOBJECTIVESUBJECTTOTHEIRSLOCALDESIGNCONSTRAINTSTHEINVOLVINGOFAUXILIARYDESIGNVARIABLESCONSISTENCYCONSTRAINTSPROVIDESAWAYTODECOUPLETHEDISCIPLINESMAKESTHEPARALLELSUBSYSTEMOPTIMIZATIONPOSSIBLESURROGATEMODELSAREUSEDINAERODYNAMICSTRUCTURALANALYSISINDERTOREDUCETHEDIFFICULTYIMPROVETHECOMPUTINGSPEEDTHERESEARCHPROVESTHATTHEMULTIDISCIPLINARYDESIGNOPTIMIZATIONMETHODCANEFFICIENTLYDECREASETHETAKEOFFWEIGHTOFTHEAIRCRAFTTHISTHESISALSOINVESTIGATEDTHEEFFECTOFSOMEOVERALLPARAMETERSONTAKEOFFWEIGHTTHEDESIGNPROCESSESAREACCOMPLISHEDAUTOMATICALLYUSINGTHEGENERALOPTIMIZATIONSOFTWAREISIGHTTHEDESIGNCYCLECANBESHTEDWITHTHEAIDOFTHESOFTWAREISIGHTKEYWDSSOLARPOWEREDAIRCRAFTOPTIMIZATIONAERODYNAMICDESIGNSTRUCTURALDESIGNAIRCRAFTDESIGN

簡介：南京航空航天大學(xué)碩士學(xué)位論文聯(lián)接翼飛機結(jié)構(gòu)重量分析與氣動結(jié)構(gòu)一體化設(shè)計姓名王小妮申請學(xué)位級別碩士專業(yè)飛行器設(shè)計指導(dǎo)教師余雄慶20050101鍪篷墨堡整蹩量笙童童冬墊燕塑二堡簍鍪生ABSTRACT髓EJOINEDWINGISANINNOVATIVEAIRCRAFTCONFIGURATIONWITHASTRUCTURALCONNECTIONBETWEENTHEFRONTWINGANDTHEREAL“WINGSUCHCONFIGURATIONSHAVESEVERALPOTENTIALADVANTAGESINCLUDINGSTRUCTURALWEIGHTREDUCTION，HIGHSTIFFNESS，LOWINDUCEDDRAG，HIGHTRIMMEDMAXIMUMLIRCOEFFICENT，REDUCEDWETTEDAREAANDPARASITEDRAG，DIRECTLIFTCONTROLCAPABILITYDIRECTSIDEFORCECONTROLCAPABILITY，GOODSTABILITYANDCONTROLCHARACTERIDTICSTHEREFORE，MANYSPECIALISTSAREAARACTEDTOSTUDYTHECONCEPTOFJOINEDWINGSTHISPAPERPRESENTEDAMETHODINVESTIGATINGTHERELATIONSBETWEENHIGHASPECTRATIOJOINEDWINGCONFIGURATIONPARAMETERANDITSWINGSTRUCTURALWEIGHTTHOSEREAHIONSISESSENTIALFORPRILIMINARYDEISGNOFTHEJOINEDWINGTHEJOINEDWINGSTRUCTURALWEIGHTSWEREPREDICATEDBYTHECOMBINATIONOFPARAMETERIZEDMODELINGOFTHEFINITEELEMENTMETHODFEMWITHSTRUCTUREOPTIMIZATIONMETHOD，ANDTHEQUANTITATIVERELATIONSBETWEENJOINEDWINGCONFIGURATIONPARAMETERSANDSTRUCTURALWEIGHTSWEREFOUNDOUTUSINGTHEDESIGNOFEXPERIMENTDOEMETHODANDRESPONSESURFACESMODELTHESTUDYRESULTSINDICATEDTHISMETHODWASABLETOFINDOUTTHERELATIONSBETWEENTHECONFIGURATIONOFJOINEDWINGSANDITSSTRUCTURALWEJI馥THOSERELATIONSCANBEUSEDASAGUIDANCETOSIZEPARAMETERSOFTHEJOINEDWINGCONFIGURATIONTHEESSENCEOFTHECONCEPTOFJOINEDWINGSISTHEINTEGRATIONOFITSSTRUCTUREANDAERODYNAMICSTHEBESTWAYTOOBTAINANOPTIMUMDESIGNISBYACCOUNTINGTHESTRUCTURALANDAERODYNAMICCHARACTERISTICSSIMULTANEOUSLYWEINVESTIGATEDTHEJOINEDWINGINTEGRATEDDESIGNOFAERODYNAMICS／STRUCTURE，WHICHISIMPLEMENTEDUSINGISIGHTSOFTWAREKEYWORDSJOINEDWING，OPTIMIZATIONDESIGN，DESIGNOFEXPERIMENTAL，RESPONSESURFACESMODEL，INTEGRATEDDESIGN

簡介：中圖分類號V2313論文編號102870215S086學(xué)科分類號082502碩士學(xué)位論文基于推力矢量的先進概念飛機飛發(fā)一體氣動研究研究生姓名陳文學(xué)科、專業(yè)航空宇航推進理論與工程研究方向內(nèi)流空氣動力學(xué)及推進系統(tǒng)指導(dǎo)教師汪明生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一四年十二月NANJINGUNIVERSITYOFAERONAUTICSANDASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFENERGYANDPOWERENGINEERINGPRELIMINARYSTUDYONINTEGRATEDAERODYNAMICCHARACTERISTICSOFTHEAIRCRAFT/ENGINEBASEDONTHRUSTVECTORINGTECHNIQUEATHESISINAEROSPACEPROPULSIONTHEORYANDENGINEERINGBYCHENWENADVISEDBYASSOCIATEPROFESSORWANGMINGSHENGSUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFORTHEDEGREEOFMASTEROFENGINEERINGDECEMBER,2014

簡介：中國科學(xué)技術(shù)大學(xué)博士學(xué)位論文魯棒非線性導(dǎo)引與控制律一體化設(shè)計研究作者姓名學(xué)科專業(yè)導(dǎo)師姓名完成時間嚴(yán)晗控制理論與控制工程季海波教授二。一三年五月二日中國科學(xué)技術(shù)大學(xué)學(xué)位論文原創(chuàng)性聲明本人聲明所呈交的學(xué)位論文，是本人在導(dǎo)師指導(dǎo)下進行研究工作所取得的成果。除已特別加以標(biāo)注和致謝的地方外，論文中不包含任何他人已經(jīng)發(fā)表或撰寫過的研究成果。與我一同工作的同志對本研究所做的貢獻均已在論文中作了明確的說明。作者簽名翌墮簽字日期壟壘7中國科學(xué)技術(shù)大學(xué)學(xué)位論文授權(quán)使用聲明作為申請學(xué)位的條件之一，學(xué)位論文著作權(quán)擁有者授權(quán)中國科學(xué)技術(shù)大學(xué)擁有學(xué)位論文的部分使用權(quán)，即學(xué)校有權(quán)按有關(guān)規(guī)定向國家有關(guān)部門或機構(gòu)送交論文的復(fù)印件和電子版，允許論文被查閱和借閱，可以將學(xué)位論文編入中國學(xué)位論文全文數(shù)據(jù)庫等有關(guān)數(shù)據(jù)庫進行檢索，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。本人提交的電子文檔的內(nèi)容和紙質(zhì)論文的內(nèi)容相一致。保密的學(xué)位論文在解密后也遵守此規(guī)定。0公開口保密年作者簽名乏墮簽字日期丕墮613導(dǎo)師簽名簽字日期

簡介：南京航空航天大學(xué)碩士學(xué)位論文雙喉道射流矢量噴管的設(shè)計規(guī)律及與后機身一體化的探索姓名陳智申請學(xué)位級別碩士專業(yè)動力機械及工程指導(dǎo)教師譚慧俊20070101雙喉道射流矢量噴管的設(shè)計規(guī)律及與后機身的一體化的探索IIABSTRACTUSINGCFDDOEANOPTIMIZATIONSTUDYFA2DDUALTHROATFLUIDICTHRUSTVECTINGNOZZLEISPERFMEDBASEDONTHEOPTIMIZATIONRESULTSANOPTIMALTHREEDIMENSIONALNOZZLEISDESIGNEDTHENTHEEFFECTSOFTHEAIRCRAFTAFTERBODYONTHEPERFMANCEOFTHENOZZLEAREOBTAINEDINTHISPAPERINDERTOIMPROVETHEPOPERFMANCEOFTHENOZZLEWITHTHEAFTERDECKCAUSEDBYTHEINTEGRATIONWITHTHEAFTERBODYONEMETHODBYPLACINGSLOTSONTHEAFTERDECKISBROUGHTFWARDNUMERICALLYSTUDIEDINADDITIONWITHTHEAIMOFTHEHIGHRESOLUTIONSOFTHEEXPERIMENTANIMPROVEDDESIGNFTHETESTFACILITYISCONDUCTEDTHERELIABILITIESISPROVEDBYUNCERTAINTYANALYSISRESULTSSHOWLENGTHOFPRIMARYNOZZLECAVITYDIVERGENTCAVITYRAMPANGLECONVERGENTCAVITYRAMPANGLEHEIGHTOFPRIMARYNOZZLEUPSTREAMTHROATSECONDARYFLOWINJECTIONANGLEAFFECTTHEPERFMANCEINTERNALFLOWPATTERNSOFTHENOZZLEOBVIOUSLYTHEOPTIMALDESIGNCANACHIEVEAPITCHTHRUSTVECTANGLEOF1434ODEGREESATAMASSCONSUMPTIONOF255?RESPONDINGTHRUSTRATIOOF0967FURTHERMEDUETOTHEINTEGRATIONWITHTHEAFTERBODYOBVIOUSBADINFLUENCESAREBROUGHTONTHEPERFMANCEOFTHENOZZLEWITHTHEAFTERDECKSWEPTANGLETHEREEONEMETHODTHATPLACESTHESLOTSONTHEAFTERDECKISBROUGHTFWARDTOIMPROVETHEPOPERFMANCEOFTHENOZZLEWITHTHEAFTERDECKTHECFDRESULTSINDICATETHATUSINGTHISMETHODATTHECRUISECONDITIONTHETHRUSTCOEFFICIENTCANBERAISEDTO095THECRESPONDINGVECTANGLEISREDUCEDTO2OWITHOUTTHEINJECTIONADDITIONALLYANIMPROVEDDESIGNFTHEBASELINETESTFACILITYISCONDUCTEDTHESYSTEMUNCERTAINTYISLOWEREDFROM2TO05KEYWDSDUALTHROATFLUIDICTHRUSTVECTINGNOZZLEAFTERBODYAFTERDECKSWEPTDOE

簡介：碩士學(xué)位論文碩士學(xué)位論文↑（航天器一體化電源的三端口DCDC變換器研究↑（RESEARCHONTHREEPTCONVERTEROFINTEGRATEDPOWERSUPPLYFSPACECRAFT↑（張藝張藝↑（哈爾濱工業(yè)大學(xué)哈爾濱工業(yè)大學(xué)2014年6月宋CLASSIFIEDINDEXTM46UDC6213DISSERTATIONFTHEMASTERDEGREEINENGINEERING↑（RESEARCHONTHREEPTCONVERTEROFINTEGRATEDPOWERSUPPLYFSPACECRAFT↑（CIDATEZHANGYISUPERVISASSOPROFWANGHONGACADEMICDEGREEAPPLIEDFMASTEROFENGINEERINGSPECIALITYELECTRICALENGINEERINGAFFILIATIONSHENZHENGRADUATESCHOOLDATEOFDEFENCEJUNE2014DEGREECONFERRINGINSTITUTIONHARBININSTITUTEOFTECHNOLOGY（

簡介：西北工業(yè)大學(xué)碩士學(xué)位論文高超聲速飛行器機體發(fā)動機一體化設(shè)計研究姓名徐華松申請學(xué)位級別碩士專業(yè)飛行器設(shè)計指導(dǎo)教師谷良賢20060301西北工業(yè)大學(xué)碩士學(xué)僚論文ABSTRACTABSTRACTHYPERSONICVEHICLEMUSTBEDESIGNEDININTEGRATIONMETHODOLOGYFORTHESTRONGCOUPLINGEFFECTOFTHESUBSYSTEMSINTEGRATEDDESIGNMETHODOLOGYOFAIRFRAME／ENGINEISTHEMOSTIMPORTANTSTEPOFINTEGRATIONMETHODOLOGYTHEAIRFRAME／ENGINEINTEGRATIONISSUESARESTUDIESINTHISPAPERBYMEANSOFTHEORETICALANALYSISANDNUMERICALSIMULATIONTHEBASICTHEORYOFNUMERICALSIMULATIONISINTRODUCEDANDTHEDESIGNEDCONFIGURATIONOFHYPERSONICVEHICLEISCHOSENTHEAERODYNAMIC／PROPULSIVEINTERFACEAPIANDENGINE／AIRFRAMEINTERFACEEAIAREPLOTTEDTHEINTEGRATIONPERFORMANCEISANALYZEDUSINGNUMERICALSIMULATIONMETHODTHEEFFECTOFWEDGESWITHDIFFERENTCOMPRESSEDANGLESONFOREBODY／INLETPERFORMANCEISANALYZEDUNDERDESIGNEDCONDITIONSTHEFOREBODYCONFIGURATIONISDESIGNEDWITHTHERESTRICTIONOFTOTALPRESSURERECOVERYCOEFFICIENTANDDRAGCOEFFICIENTTHECHANGESOFFLOWFIELDOFFOREBODY／INLETAREANALYZEDUNDERDESIGNEDCONDITIONSANDUNDERSIGNEDCONDITIONSTHEPARAMETERDESIGNMETHODOFNOZZLEAFTERBODYISINTRODUCEDTHEINTERNALPORTIONOFNOZZLEAFTERBODYISDESIGNEDUSINGTHETHEORYOFEXPANSIONWAVETHEUPPERWALLISDESIGNEDFORBERERTHRUSTCOEFFICIENTTHEPROPULSIONPERFORMANCEOFNOZZLEAFLERBODYISIMPROVEDKEYWORDHYPERSONIC；AIRFRAME／ENGINEINTEGRATION；NUMERICALSIMULATION；FOREBUDY；NOZZLEAFTERBODY

簡介：分類號V4482學(xué)號10019057ＵＤＣ密級公開工學(xué)博士學(xué)位論文航天器相對運動姿軌一體化動力學(xué)航天器相對運動姿軌一體化動力學(xué)建模與控制技術(shù)研究建模與控制技術(shù)研究博士生姓名吳錦杰學(xué)科專業(yè)航空宇航科學(xué)與技術(shù)研究方向飛行器動力學(xué)與控制指導(dǎo)教師劉昆教授國防科學(xué)技術(shù)大學(xué)研究生院國防科學(xué)技術(shù)大學(xué)研究生院二〇一三年九月二〇一三年九月RESEARCHONATTITUDEBITINTEGRATEDDYNAMICSMODELINGCONTROLTECHNOLOGIESFSPACECRAFTRELATIVEMOTIONCIDATEWUJINJIESUPERVISPROFLIUKUNADISSERTATIONSUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFTHEDEGREEOFDOCTOFENGINEERINGINAERONAUTICALASTRONAUTICALSCIENCETECHNOLOGYGRADUATESCHOOLOFNATIONALUNIVERSITYOFDEFENSETECHNOLOGYCHANGSHA，HUNAN，PRCHINASEPTEMBER，2013

簡介：中圖分類號V2453論文編號102870215S045學(xué)科分類號082502碩士學(xué)位論文飛機綜合一體化熱能量管理系統(tǒng)方案研究研究生姓名雷屹坤學(xué)科、專業(yè)航空宇航推進理論與工程研究方向傳熱與傳質(zhì)指導(dǎo)教師常海萍教授南京航空航天大學(xué)研究生院能源與動力學(xué)院二〇一四年十二月NANJINGUNIVERSITYOFAERONAUTICSASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFENERGYPOWERENGINEERINGRESEARCHONSCHEMEOFINTEGRATEDTHERMALENERGYMANAGEMENTSYSTEMOFAIRCRAFTATHESISINAEROSPACEPROPULSIONTHEYENGINEERINGBYLEIYIKUNADVISEDBYPROFCHANGHAIPINGSUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFTHEDEGREEOFMASTEROFENGINEERINGDECEMBER2014

簡介：工學(xué)碩士學(xué)位論文驅(qū)動轉(zhuǎn)向一體化車輪轉(zhuǎn)向特性分析與結(jié)構(gòu)研究尹甲人哈爾濱工業(yè)大學(xué)2008年6月CLASSIFIEDINDEXV4763UDC629785ADISSERTATIONFTHEDEGREEOFMENGSTEERINGACTERANALYSISSTRUCTURERESEARCHFINTEGRATEDWHEELDRIVINGSTEERINGCIDATEYINJIARENSUPERVISASSOCIATEPROFGAOHAIBOACADEMICDEGREEAPPLIEDFMASTEROFENGINEERINGSPECIALTYMACHINEDESIGNTHEYDATEOFALEXAMINATIONJUNE2008UNIVERSITYHARBININSTITUTEOFTECHNOLOGY

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簡介：南京理工大學(xué)碩士學(xué)位論文固體燃料沖壓增程彈內(nèi)外彈道一體化計算研究姓名蔣波申請學(xué)位級別碩士專業(yè)武器系統(tǒng)與運用工程指導(dǎo)教師武曉松20090501ABSTRACT碩士論文ABSTIUCTSFRJISAKINDOFNEWTYPEPROPULSIONSYSTEMWHICHPOSSESSESTHEVIRTUEOFSIMPLESTRUCTURE，HIGHSPECIFICIMPULSEANDACCOMMODATINGTHEGASFLUXITSELFTHEENDPOINTVELOCITYANDPERFORMANCEOFTHEPROJECTILEISENORMOUSLYIMPROVEDBYTHEUSEOFSFRJTHESFRJPROJECTILEHASVERYNICEPROSPECTSTHEPAPERISMAINLYABOUTTHEEVALUATIONOFTHESOLIDFUELRAMJETPROPELLEDPROJECTILE’SBALLISTICTRAJECTORYPERFORMANCETHERANGEEXTENDEDTHEORYOFARAMJETPROPELLEDPROJECTILEISPRESENTED，ANDTHEBALLISTICTRAJECTORYPREDICTIONMODELISESTABLISHEDBASEDONTHEMODEL，ASPECIALCOMPUTERPROGRAMISCOMPILEDTOFIGUREOUTTHETRAJECTORYPERFORMANCEOFPROJECTILETHEPROGRAMCOULDNOTONLYBEUSEDFORPROJECTILEPERFORMANCECOMPUTATION，BUTALSOBEUSEDFORDESIGNOFTHERAMJETPROPELLEDPROJECTILEASTOREALIZEQUICKDESIGNANDPERFORMANCEANALYSISTHETRAJECTORYPROJECTILEISNUMERICALLYSIMULATED，THROUGHANALYSINGTHERESTS，THERELATIONSAREATTAINEDINADDITION，THERESEARCHANDRESULTASWELLASTHEPROCEDUREINTHISARTICLEWILLPROVIDECERTAINTHEORYINSTRUCTIONANDTHEREFERENCEVALUEFORTHEDESIGNANDEXPERIMENTOFTHESOLIDFUELRAMJETKEYWORDSSOLIDFUELRAMJETSFRJ，ADVANCEMENTTECHNIQUESOFPROPULSIONPERFORMANCEOFBALLISTICTRAJECTORYRANGEEXTENDEDⅡ

簡介：分類號密級UDC編號工學(xué)碩士學(xué)位論文超燃燃燒室支板構(gòu)型及支板凹腔一體化數(shù)值研究碩士研究生茍東亮指導(dǎo)教師朱衛(wèi)兵教授學(xué)科、專業(yè)航空宇航科學(xué)與技術(shù)論文主審人王革教授分類號密級UDC編號工學(xué)碩士學(xué)位論文超燃燃燒室支板構(gòu)型及支板凹腔一體化數(shù)值研究碩士研究碩士研究生茍東亮指導(dǎo)教師指導(dǎo)教師朱衛(wèi)兵教授學(xué)位級別學(xué)位級別工學(xué)碩士學(xué)科、專學(xué)科、專業(yè)航空宇航科學(xué)與技術(shù)所在單位所在單位航天與建筑工程學(xué)院論文提交論文提交日期日期2014年12月24號