Journal of Propulsion Technology 1999 Issue 3 tong yong fa dong ji / wei kang mu si lian he yan zhi xiao xing wo lun fa dong ji

tong yong fa dong ji / wei kang mu si lian he yan zhi xiao xing wo lun fa dong ji

..............page:94

mei hang kong pen qi fa dong ji gong si jie shou gao chao sheng su dao dan yong tui jin xi tong ren wu

..............page:52

SURVEY OF INTERNAL PROCESS STUDIES ON ARCJET THRUSTERS
Liao Hongtu;Wu Minglan;Wang Nanhao

..............page:107

STUDY ON ZERO POINT VARIATION OF SOLID ROCKET ENGINE TESTING SYSTEM
Zhang Junyue;Ren Min;Zhou Guilan

..............page:103-106

STUDIES ON MORPHOLOGICAL STRUCTURE OF HIGHLY PLASTICIZED POLYETHYLENE GLYCOL POLYURETHANE ELASTOMER
Hong Xiaobin;Du Lei;Zhang Xiaoping

..............page:100-102

EFFECT OF PROPELLANT COMPONENTS ON DEGRADATION OF POLYETHER-URETHANE BINDER (Ⅱ)EFFECTS OF ENERGETIC FILLERS AND ADDITIVES
Luo Shanguo;Chen Futai;Luo Yunjun;Tan Huimin;Man Guanglei;Guo Yanwen;Zhang Jianguo

..............page:95-99

STUDY OF DSMC METHOD FOR EXHAUST PLUME IMPINGEMENT EFFECTS ON SPACECRAFT SURFACES
Huang Lin;Wu Qifen;Ren Bing

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

SENSITIVITY ANALYSIS OF SSTOVEHICLE PARAMETERS
Huang Yiyong;Zhang Yulin

..............page:10-12

START-UP SIMULATION OF A LIQUID PROPELLANT STAGED COMBUSTION ROCKET ENGINE
Liu Hongjun;Zhang Enzhao;Dong Xijian

..............page:5-9

NUMERICAL SIMULATION OF HEAT TRANSFER IN TRANSPIRATION COOLED LIQUID ROCKET THRUSTER CHAMBER(Ⅰ) PHYSICAL-MATHEMATICAL MODEL
Jiang Peixue;Ren Zepei;Zhang Zuofan;Chen Xuyang

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

RELATIVITY STUDY ON PYROLYTIC CHARACTERISTICS AND CATALYTIC ACTIVITIES OF SOME NTO SALTS IN SOLID PROPELLANT
Guan Dalin;Li Shangwen;Yin Cuimei;Zhang Shuangjian;Dang Yongzhan

..............page:91-94

STUDY ON THERMAL DECOMPOSITION CHARACTERISTICS OF GAP/AN PROPELLANT
Zhao Xiaobin;Hou Linfa;Zhang Xiaoping

..............page:86-90

COMBUSTION PROPERTIES OF HTPB PROPELLANTS WITH BURNING RATE CATALYSTS AT HIGH PRESSURE
Xu Haoxing;Lu Guolin;Zhao Xiuyuan

..............page:81-85

RESEARCH OF CAD TECHNOLOGY IN AEROENGINE DESIGN
Guo Shufen;jia Bo

..............page:78-80

SOLUTION OF PARAMETRIC RICCATI EQUATION ON TURBOJET ENGINE H∞ CONTROL
Wang Xi;Xie Zhenhua;Zeng Qingfu

..............page:73-77

EXPERIMENT STUDY ON EFFECT OF TIP CLEARANCE ON CENTRIFUGAL IMPELLER PERFORMANCE
Chu Wuli;Liu Zhiwei

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

EFFECTS OF INLET FLOW CONDITIONS ON BOUNDARY FLOW ON COMPRESSOR BLADE SURFACE
Liu Bo;Wang Yangang;Xiao Min

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

EXPERIMENT MODAL ANALYSIS ON FRONT BEARING SPRING SUPPORT FOR TURBOJET ENGINE
Sun Yang

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

COMPUTATION OF DUAL-MODE SUPERSONIC COMBUSTOR
Lu Yanhong;Ling Wenhui;Liu Jinghua;Ye Zhongyuan;Ma Xianghui

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

STUDY ON STRUCTURAL AGEING RELIABILITY FOR FLEXIBLE JOINT OF SOLID ROCKET MOTOR
Liu Yongqiong;Wang Liang

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

TWO-DIMENSIONAL AND TWO-PHASE COLD FLOW TEST IN ENTRANCE REGION OF SUBMERGED NOZZLE
He Hongqing;Yao Na;He Guoqiang;Wang Simin;Zhang Zhaoyuan;Cai Timin

..............page:50-52

PARAMETERS IDENTIFICATION OF ALKALI METAL IMPURITIES OF SOLID PROPELLANT AND PROPERTIES OF EXHAUST AFTERBURNING
Liu Qingyun;Zhang Ping;An Dongmei

..............page:45-49

INVESTIGATION OF SIDEWALL COMPRESSION INLET WITH CONSTANT PRESSURE RATION AND CURVED LEADING EDGE UNDER NONUNIFORM SUPERSONIC FLOW
Zhang Kunyuan;Ma Yanrong;Xu Hui

..............page:40-44

NUMERICAL ANALYSIS OF CONVECTIVE BURNING FLOW FIELD IN PROPELLANT CRACK
Li Jiang;He Guoqiang;Cai Timin

..............page:36-39

EXPERIMENTAL STUDY OF ANOMALOUS COMBUSTION IN SOLID PROPELLANT GRAIN WITH DEFECTS
He Guoqiang;Cai Timin;Li Jiang;Liu Peijin;Du Lei;Sun Fengzhou;Tan Jianbo

..............page:30-35

STUDY ON ENGINE MILITARY REGIME CONTROL FOR ADVANCED FIGHTER
Tang Diyi;Tu Qiuye

..............page:25-29

EXPERIMENTAL INVESTIGATION ON DETONATIVE RANGE,INNER FLOW GAS TEMPERATURE AND WALL TEMPERATURE OF PULSED DETONATION ENGINE
He Liming;Yan Chuanjun;Fan Wei;Lei Hengren

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

NUMERICAL STUDIES FOR INTERACTION FLOWFIELD BETWEEN SUPERSONIC FLOW AROUND BODY AND JET FLOW EXHAUSTING FROM ROCKET
Ju Yutao;Zheng Ya

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