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(jì)劃一體化處理系統(tǒng)的設(shè)計(jì)與實(shí)現(xiàn)摘要飛行計(jì)劃的一體化處理就是實(shí)現(xiàn)飛行計(jì)劃的統(tǒng)一申請(qǐng)、統(tǒng)一生成、統(tǒng)一更新和統(tǒng)一發(fā)布，解決目前飛行計(jì)劃由各管制中心單獨(dú)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(jì)劃數(shù)據(jù)服務(wù)。飛行計(jì)劃一體化處理是對(duì)現(xiàn)有民航飛行計(jì)劃管理模式的一次革命性改進(jìn)，對(duì)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(jì)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(duì)飛行計(jì)劃一體化處理進(jìn)行技術(shù)論證。民航華北空管局依據(jù)對(duì)飛行計(jì)劃一體化的理解，結(jié)合自身飛行計(jì)劃管理的特點(diǎn)，提出了區(qū)域飛行計(jì)劃一體化處理的需求，并與中國電子科技集團(tuán)公司第二十J、研究所合作進(jìn)行民航華北地區(qū)飛行計(jì)劃一體化處理系統(tǒng)設(shè)計(jì)開發(fā)。本文結(jié)合民航華北地區(qū)飛行計(jì)劃一體化處理系統(tǒng)的系統(tǒng)研制過程，重點(diǎn)論述了經(jīng)用戶確認(rèn)的系統(tǒng)設(shè)計(jì)及實(shí)現(xiàn)方案，并對(duì)系統(tǒng)的關(guān)鍵技術(shù)和系統(tǒng)結(jié)論進(jìn)行了論述。關(guān)鍵詞飛行計(jì)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(jī)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(duì)本學(xué)位論文做出的貢獻(xiàn)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(jī)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(duì)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(jī)氣動(dòng)結(jié)構(gòu)推進(jìn)一體化設(shè)計(jì)研究姓名鄧海強(qiáng)申請(qǐng)學(xué)位級(jí)別碩士專業(yè)飛行器設(shè)計(jì)指導(dǎo)教師余雄慶20061201小型太陽能飛機(jī)氣動(dòng)結(jié)構(gòu)推進(jìn)一體化設(shè)計(jì)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(jī)結(jié)構(gòu)重量分析與氣動(dòng)結(jié)構(gòu)一體化設(shè)計(jì)姓名王小妮申請(qǐng)學(xué)位級(jí)別碩士專業(yè)飛行器設(shè)計(jì)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(hào)V2313論文編號(hào)102870215S086學(xué)科分類號(hào)082502碩士學(xué)位論文基于推力矢量的先進(jìn)概念飛機(jī)飛發(fā)一體氣動(dòng)研究研究生姓名陳文學(xué)科、專業(yè)航空宇航推進(jìn)理論與工程研究方向內(nèi)流空氣動(dòng)力學(xué)及推進(jìn)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(dòng)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(jì)研究作者姓名學(xué)科專業(yè)導(dǎo)師姓名完成時(shí)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(jìn)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(duì)本研究所做的貢獻(xiàn)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(qǐng)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(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，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(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。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(jì)規(guī)律及與后機(jī)身一體化的探索姓名陳智申請(qǐng)學(xué)位級(jí)別碩士專業(yè)動(dòng)力機(jī)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(jì)規(guī)律及與后機(jī)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(jī)體發(fā)動(dòng)機(jī)一體化設(shè)計(jì)研究姓名徐華松申請(qǐng)學(xué)位級(jí)別碩士專業(yè)飛行器設(shè)計(jì)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(hào)V4482學(xué)號(hào)10019057ＵＤＣ密級(jí)公開工學(xué)博士學(xué)位論文航天器相對(duì)運(yùn)動(dòng)姿軌一體化動(dòng)力學(xué)航天器相對(duì)運(yùn)動(dòng)姿軌一體化動(dòng)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(dòng)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(hào)V2453論文編號(hào)102870215S045學(xué)科分類號(hào)082502碩士學(xué)位論文飛機(jī)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(jìn)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(dòng)力學(xué)院二〇一四年十二月NANJINGUNIVERSITYOFAERONAUTICSASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFENERGYPOWERENGINEERINGRESEARCHONSCHEMEOFINTEGRATEDTHERMALENERGYMANAGEMENTSYSTEMOFAIRCRAFTATHESISINAEROSPACEPROPULSIONTHEYENGINEERINGBYLEIYIKUNADVISEDBYPROFCHANGHAIPINGSUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFTHEDEGREEOFMASTEROFENGINEERINGDECEMBER2014

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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(jì)算研究姓名蔣波申請(qǐng)學(xué)位級(jí)別碩士專業(yè)武器系統(tǒng)與運(yùn)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(hào)密級(jí)UDC編號(hào)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(hào)密級(jí)UDC編號(hào)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(jí)別學(xué)位級(jí)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(hào)