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1.
FATIGUEDISLOCATIONCONFIGURATIONSINHEXAGONALZIRCALOY-4¥XiaoLin(InstituteofEngineeringMech.,Xi'anJiaotongUniversity,Xi'an,China...  相似文献   

2.
EXPERIMENTALSTUDYONTHEINFRAREDRADIATIONCHARACTERISTICSFROMHOTJETShanQixiang;BuMan(CollegeofScience,NanjingUniversityofAeronau...  相似文献   

3.
高歌  熊焰 《航空动力学报》1996,11(4):401-405,439
TRANSITIONSIMULATIONUSINGGLM-EMBASEDCLOSEDEQUATIONSOFTURBULENCEGaoGe(4thDept.BeijingUniversityofAeronauticsandAstronautics,Be...  相似文献   

4.
PARAMETRICSHIMMYANALYSISZhouJinxiong(周进雄),ZhuDepei(诸德培)(Dept.ofAircraftEnginering,NorthwesternPolytechnicalUniversity,Xi′an,7...  相似文献   

5.
hyperMILL是一款集成化2D/3D的CAM解决方案,它可以集成于Autodesk的Mechanical Desktop~TM,think3的thinkde-sign, Dassault的CATIA以及CoCreate的SolidDesigner等环境内。在这些熟悉的软件环境下,用户可以直接将这些CAD设计转变为用于加工的NC代码。  相似文献   

6.
INVESTIGATIONONCONTROLOFCHAOSYuJianzu(Dept.ofFlightVehicleDesignandAppliedMechanics,BeijingUniversityofAeronauticsandAstronau...  相似文献   

7.
ESTIMATIONOFFATIGUELIFEUNDERRANDOMLOADINGWITHPLASTICHYSTERESISENERGYTHEOREMWuFumin(NorthwesternPolytechnicalUniversity,Xi'an,...  相似文献   

8.
EXPERIMENTAL STUDY OF TURBULENT WINGBODY JUNCTION AND WAKEFLOWKangHongwen;FanMeng;WeiZhonglei(DepartmentofMechanics,PekingUni...  相似文献   

9.
《中国航空学报》1999,12(4):24-229
ABSTRACTS(Vol.20,No.3)Pre-postbucklinganalysisofcompositelaminateswithdelaminationdamage.SUNXian-nian,CHENHao-ran(DepartmentofEngineeringMechanicsofDalianUniversityofTechnology,Dalian116023,China),CHENShao-jie(ShengyangAircraftResearchInstitute,Sheny…  相似文献   

10.
HIGHORDERACCURACYSCHEMEFOR2-DTRANSONICFLOWS¥LiHaidong;LiuQiusheng;ShenMengyu(DepartmentofEngineeringMechanics,TsinghuaUnivers...  相似文献   

11.
RELIABILITYANDDAMAGETOLERANCEANALYSISFORAIRCRAFTPROPELLERFeiBinjun,GaoZhentong(InstituteofSolidMechanics,BeijingUniversityofA...  相似文献   

12.
ANALYTICALMODELOFHELICOPTERAIRCOMBATANDMATHEMATICINVERSESOLUTIONCaoYihua(InstituteofFluidMechanics,BeijingUniversityofAeronau...  相似文献   

13.
EXPERIMENTALRESEARCHONSTRESSINTENSITYFACTORKⅢFOR3┐DCRACKBYCAUSTICSWuDafang,GaoZhentong(InstituteofSolidMechanics,BeijingUnive...  相似文献   

14.
NUMERICAL SIMULATION OF VORTEX BREAKDOWN ON A DELTA WING AT LOW SPEEDZhuZiqiang;JiaJianbo(InstituteofFluidMechanics,BeijingUn...  相似文献   

15.
BSTRACTSConflictProblemofDempster ShaferEvidenceTheory .ZHANGShan ying ,PANQuan ,ZHANGHong cai(Depart mentofAutomaticControl,NorthwesternPolytechnicUni versity ,Xi′an  710 0 72 ,China) .ActaAeronauticaetAs tronauticaSinica (ISSN 10 0 0 6 893) ,Vol.2 2 ,no .4 ,July2 0 0 1,P36 9 372 .13refs…  相似文献   

16.
ANANALYSISOFPROPELLERLIFTING-LINETHEORYBYMATCHEDASYMPTOTICEXPANSIONSChenZemin;PanJieyuan;WuLiyi(InstituteofFluidMechanics,Bei...  相似文献   

17.
FUZZYPETRINETFORFAULTDIAGNOSISWuyanfang;WeiZhongxin.(DepartmentofMechanicalEngineering,NanjingUniversityofAeronauticsandAstro...  相似文献   

18.
THERMALREGULATIONOFHEADREGIONANDITSSELECTIVECOOLINGPangCheng;GuDingliang(InstituteofSpaceMedico-Engineering,Beijing,China,100...  相似文献   

19.
EFFECTS OF VECTORING JET ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT   总被引:2,自引:0,他引:2  
EFFECTSOFVECTORINGJETONAERODYNAMICCHARACTERISTICSOFAIRCRAFTWANGYankui(王延奎),DENGXueying(邓学蓥)(InstituteofFluidMechanics,Beijing...  相似文献   

20.
MULTISENSORTRACKINGSYSTEMWITHATTITUDEMEASUREMENTSDingChibiao,MaoShiyi(DepartmentofElectronicEngineering,BeijingUniversityofAe...  相似文献   

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