Journal of Propulsion Technology 1999 Issue 2 fa dong ji wen ti shi x-33 shou ci fei xing tui chi

fa dong ji wen ti shi x-33 shou ci fei xing tui chi

..............page:68

..............page:60

NUMERICAL SIMULATIONS OF MIXING ENHANCEMENT OF RAMP INJECTORS IN SCRAMJET COMBUSTOR
Liang Jianhan;Wang Zhenghua;Wang Chengyao

..............page:49-52

FUZZY RELIABILITY DESIGN AND ESTIMATION METHOD FOR LONG LIFE-SPAN TURBOPUMP
Guo Fengying;He Hongqing;Li Baosheng

..............page:45-48

STUDY ON CRITICAL ROTATIONAL SPEED OF TURBOPUMP ROTORS(Ⅲ)FOR TURBOPUMP ROTORS TAKING ACCOUNT OF LIQUID ACTING FORCES
He Hongqing;Zhang Xiaolong;Shen Dakuan;Zhang Zhewen

..............page:42-44

NUMERICAL SIMULATION OF TWO DIMENSIONAL TRANSONIC TWO-PHASE TURBULENT FLOW IN NOZZLE
Yan Hong;He Hongqing

..............page:37-41

MECHANICS ANALYSIS ON THE SPATIAL MECHANISM OF DOUBLE EXTENDIBLE NOZZLE
Yan Deyuan;Zhang Yanyu;Zhang Jingsheng;Zhang Xiaohong;Cao Zhengjing;Li Yanrong

..............page:33-36

NUMERICAL SIMULATION STUDY OF SCRAMJET FLOW FIELD
Liu Jinghua;Ling Wenhui;Ma Xianghui;Liu Ling;Zhang Zhen;Wang Xinyue

..............page:28-32

STORAGE AND RESTORATION OF STANDARD SIGNAL OF AERIAL ENGINE
Xie Shousheng;Fan Siqi;Duan Shoufu

..............page:25-27

STUDY ON STARTUP MODEL AND STARTUP CONTROL LAW OF TURBOFAN ENGINE
Tu Qiuye;Tang Diyi

..............page:21-24

OPTIMAL DESIGN OF ACCELERATING CONTROL LAW FOR VARIABLE GEOMETRY TURBOFAN ENGINE
Ding Kaifeng;Fan Siqi

..............page:17-20

EFFECT OF THRUST BIAS AND GRAIN INITIAL TEMPERATURE ON RANGE AND CROSSWISE DEVIATION OF SPINNING ROCKET
Liu Wen;Zhang Weihua;Zhou Luojin;Zeng Qinhua

..............page:13-16

ADVANCED MODEL OF STATIC CHARACTERISTIC FOR LIQUID OXYGEN/KEROSENE PROPELLANT STAGED COMBUSTION ROCKET ENGINE
Liu Hongjun

..............page:9-12

NUMERICAL ANALYSIS OF ACOUSTICAL WAVE-MOTION IN COMBUSTION CHAMBER OF LIQUID ROCKET ENGINE
Hong Xin;Cheng Huier

..............page:5-8

NEURAL NETWORK APPROACH TO FAULT DETECTION OF LIQUID ROCKET ENGINE (Ⅱ)PATTERN RECOGNITION TECHNOLOGY
Huang Minchao;Zhang Yulin;Chen Qizhi

..............page:1-4

SUMMARY OF TYPIC LABORATORY AND TEST ABOUT LIQUID ROCKET ENGINE
Cai Guobiao;Liu Shijian;Zhang Zhenpeng

..............page:108

REVIEW OF AIRFRAME/INLET INTEGRATION OF MANEUVER FIGHTER AIRCRAFT
Yang Guocai

..............page:103-107

ANALYSIS OF SOLID PROPELLANT CONTROL THRUSTER SCHEMES FOR SMALL KKV
Li Shipeng;Zhang Ping

..............page:99-102

FLAMMABILITY LIMITS OF ALUMINUM-MAGNESIUM FUEL-RICH PROPELLANT
Zhang Wei;Zhu Hui;Xue Jingen;Fang Dingyou;Xia Zhixun;Jiang Chunlin;Wan Zhangji

..............page:95-98

EFFECT OF PROPELLANT COMPONENTS ON DEGRADATION OF POLYETHER-URETHANE BINDER (Ⅰ)THE EFFECT OF NITRATE ESTERS
Luo Shanguo;Chen Futai;Luo Yunjun;Tan Huimin;Man Guanglei;Guo Yanwen;Zhang Jianguo

..............page:88-94

NITROGEN OXIDES--POTENTIAL OXIDANT OF ALUMINUM
Zhu Ji;Li Shufen;Jia Liwen

..............page:83-87

STUDY ON BURNING-RATE CONTROL OF LOW BURNING-RATE HTPB PROPELLANT
Cui Ruixi

..............page:77-82

SPRAY PROPERTY RESEARCH AND APPLICATION OF UNLIKE IMPINGING INJECTOR
Zhang Mengzheng;Fu Yonggui;Zhang Zeping;Li Ping

..............page:73-76

NUMERICAL SIMULATION ON ANGLE FACTOR OF OUTWARD RADIATION FOR FOUR DIAGONALLY-ARRANGED NOZZLES
Cheng Huier;Hong Xin;Lu Wancheng

..............page:69-72

EXPERIMENTAL INVESTIGATION OF FILM COOLING HEAT TRANSFER ON TURBINE BLADE LEADING EDGE
Zhu Huiren;Xu Duchun;Guo Tao;Liu Songling

..............page:64-68

SIMULATION ON FLOW AND MIXING OF TURBULENT IN DIVERGING DUCT
Zhang Jian;Zhou Lixing

..............page:61-63

ON MODEL OF STAGE-BY-STAGE DYNAMIC BLADE RESPONSE FOR PREDICTING AERODYNAMIC STABILITIES IN MULTISTAGE AXIAL COMPRESSORS WITH INLET DISTORTIONS
Wu Hu;Lian Xiaochun;Chen Fuqun

..............page:56-60

3D NUMERICAL SIMULATION OF HYPERSONIC JET INTERACTION FLOWFIELD
Li Hua;Wang Chengyao

..............page:53-55