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Journal of Propulsion Technology
1001-4055
1998 Issue 4
DEVELOPMENT OF BALANCE TECHNOLOGY FOR AEROENGINES
Chen Bingyi
..............page:105-109
DESIGN OF THE SUBMERGED INLET
Peng Chengyi;Ma Qiang;Ma Jiaju
..............page:36-40
NUMERICAL STUDY OF MIXING FLOWS IN A DUCTED ROCKET COMBUSTOR
Ma Zhibo;Zhang Zhenpeng;Cai Xuanyi
..............page:32-35
COMPENSATION TECHNOLOGY INVESTIGATION FOR IMPULSE THRUST OF SOLID ROCKET MOTOR
Wu Junsheng;Zhou Shengguo
..............page:27-31
COUPLING BETWEEN MICROWAVE AND PLASMA FLOW
Mao Genwang;Ma Hongya;He Hongqing
..............page:14-17
REVIEW OF DEHYDROGNATION CATALYSIS OF ENDOTHERMIC HYDROCARBON FUEL
Gao Han;Li Zuguang;Li Gang;Lin Ruisen
..............page:100-104
STUDY ON BURNING RATE CATALYSTS OF ULTRA-HIGH BURNING RATE PROPELLANT
Tang Songqing;Gong Hua;Yan Sihai;Miao Lin;He Fumei;Tang Dasen;Liu Xun'en;Yang Rongjie;Jing Zhongxing
..............page:91-94
REDUCTION OF MEASUREMENT UNCERTAINTY OF LIQUID PROPELLANT REMAINING ON SATELLITE BY COMBINING PVT WITH BK ORGANICALLY
Zhang Tianping;Da Daoan;Jiang Wanshun;Zhang Zhiyuan;Meng Qingping;Chen Zhen;Zhu Xiaolan;Huo Hongqing
..............page:87-90
EXPERIMENTAL INVESTIGATION OF COMPRESSOR CASCADE EXIT FLOW FIELDS WITH NEGATIVE CURVED BLADES AT DESIGN CONDITIONS
Wu Jiquan;Wu Guochuan;Su Jiexian;Zhong Jingjun;Wang Zhongqi
..............page:83-86
ESTABLISHMENT OF THE KINEMATICS PROPERTIES OF DOUBLE EXTENDIBLE NOZZLE
Yan Deyuan;Zhang Yanyu;Zhang Jingsheng;Zhang Xiaohong
..............page:70-73
NUMERICAL SIMULATION OF FLOW FIELD FOR THERMAL SEPARATION OF MULTISTAGE MISSILE
Li Jiang;Xiao Yumin;Sun Dechuan;Cai Timin
..............page:62-65
COUPLED NUMERICAL SIMULATION WITH N-S AND DSMC ON VACUUM PLUME
Cai Guobiao;Wang Huiyu;Zhuang Fenggan
..............page:57-61
STUDY ON TEST OF STREAMWISE VORTEX MIXING ENHANCEMENT
Lang Jian;Zhang Zhenjia;Zhang Jiahua
..............page:52-56
EXPERIMENTAL STUDIES ON THE INTEGRAL RAMJET WITH FOUR INLETS
Xue Guilin;Wang Jian
..............page:11-13
BIPROPELLANT MINIATURE DIVERT THRUSTER
Ge Guohua
..............page:7-10
REVIEW OF LIQUID PROPELLANT ROCKET ENGINE
Liu Guoqiu;Hu Pingxin
..............page:2-6
zhu he < tui jin ji shu > fa kan 100 qi
liu xing zhou
..............page:1