Journal of Propulsion Technology 1999 Issue 4 IMPROVEMENT OF MEASUREMENT ACCURACY OF RTR SYSTEM

IMPROVEMENT OF MEASUREMENT ACCURACY OF RTR SYSTEM
Li Jiang;Chen Jian;He Guoqiang;Cai Timin

..............page:109

STUDY ON SYNTHESIS OF HYDROXYLAMINE PERCHLORATE USING ION EXCHANGE METHOD
Chang Zhihua;Zhang Xiangwen;Mi Zhentao

..............page:105-108

REFRACTIVE INDEX INCREASE OF NITROCELLULOSE SOLUTION AFTER BEING FREEZED
Luo Yunjun;Yan Xiaohu;Tan Huimin;Qiu Wulin;Luo Shanguo

..............page:100-104

INVESTIGATION ON COMBUSTION PROPERTY OF ACCELERATED-AGING CMDB SOLID PROPELLANT
Liu Peijin;He Guoqiang;Li Jiang;Gao Ming

..............page:96-99

CALORIMETRIC SYUDY OF ENDOTHERMIC FUEL
Li Zuguang;Gao Han;Li Gang;He Zhaoyu;Lin Ruisen;Zong Hanxing

..............page:92-95

STUDY ON SAFETY PROPERTY OF GAP/AN PROPELLANT
Zhao Xiaobin;Zhang Xiaoping;Hou Linfa

..............page:89-91

EXPERIMENTAL RESEARCH ON PULSATING COMBUSTION FOR IMPROVED RIJKE COMBUSTOR
Wang Chuanfa;Wang Jiahua;Tao Lei;Zhang Donghui

..............page:85-88

EXPERIMENTAL INVESTIGATION ON TOTAL PRESSURE LOSS OF VORTEX FLAME-HOLDER WITH HOLES
Han Qixiang;Liu Hong;Wang Fang;Wang Jiahua

..............page:81-84

COMPUTATION OF COMPRESSIBLE FLOW USING RUNGE-KUTTA TIME STEPPING SCHEME
Liao Hongtu

..............page:75-80

H∞ ROBUST CONTROL OF SYSTEMS WITH STRUCTURED PERTURBATIONS BASED ON sLINEAR MATRIX INEQUALITY
Xie Guanghua;Zeng Qingfu

..............page:71-74

CONSTRUCTION OF WEIGHTING MATRIXES IN MIXED SENSITIVITIES H∞ CONTROLLER DESIGN FOR AEROENGINE
Tao Tao;Yan Wenbo

..............page:66-70

OPTIMAL DESIGN OF TWO-DIMENSIONAL COMPRESSION SURFACE UNDER NON-UNIFORM SUPERSONIC FLOW
Zhang Kunyuan;Xiao Xudong;Xu Hui

..............page:61-65

NUMERICAL SOLUATION ON VISCOUS INVERSE PROBLEM FOR TRANSONIC COMPRESSOR CASCADES
Yang Ce;Lao Dazhong;Jiang Zikang

..............page:57-60

NUMERICAL SIMULATION OF INFLUENCE OF UNSTEADY WAKE ON HEAT TRANSFER OF TURBINE BLADE
Zhu Huiren;Zhang Li;Zhou Yongcheng;Liu Songling

..............page:53-56

FAULT QUANTITATIVE DIAGNOSIS OF TURBOFAN GAS PATH COMPONENT BY BPN
Sun Bin;Zhang Jin;Zhang Shaoji

..............page:48-52

NUMERICAL SIMULATION ON THREE-DIMENSIONAL FLOWFIELD IN SLOTTED TUBE OF A HOT GAS GENERATOR
Cheng Xueling;Zhang Ping

..............page:43-47

IMPLICIT FLUX VECTOR SPLITTING METHOD OF TWO-DIMENSIONAL EQUATION WITH ADAPTIVE GRID
Yang Juan;He Hongqing;Cai Timin

..............page:40-42

ABLATION MODEL OF EPDM
He Hongqing;Yan Hong

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

STABILITY ANALYSIS OF A TURBO-PUMP EXPERIMENT SYSTEM
Liu Hongjun;Zhang Enzhao;Dong Xijian

..............page:32-35

GRIDS METHOD FOR CHAMBER-NOZZLE INTEGRATED DESIGN IN SOLID ROCKET ENGINE
Zhang Zhengke;Liu Yu

..............page:29-31

SIMULATION ON TWO-PHASE SPRAY COMBUSTION IN ROCKET ENGINE UNDER PVM ENVIRONMENT
Zhao Wentao;Wang Zhenghua;Liu Zhong;Yang Xiaodong

..............page:26-28

DYNAMIC CHARACTERISTICS DURING STARTUP AND SHUTDOWN OPERATION OF LIQUID FEED LINE COUPLED MULTI-ENGINE SYSTEM
Lin Xiqiang;Cheng Mousen;Liu Kun;Zhang Yulin;Li Wei

..............page:22-25

NUMERICAL SIMULATION OF HEAT TRANSFER IN A TRANSPIRATION COOLED LIQUID ROCKET THRUST CHAMBER (Ⅱ)NUMERICAL METHOD AND RESULTS
Jiang Peixue;Ren Zepei;Zhang Zuofan;Chen Xuyang

..............page:17-21

PRELIMINARY INVESTIGATION ON GAS DYNAMIC RESONANCE IGNITION FOR LIQUID PROPELLANT ROCKET ENGINE
Liang Guozhu;Zhang Guozhou;Cheng Xianchen;Ma Bin;Zhang Zhenpeng

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

ROCKET ENGINE DYNAMIC PROCESS MODELING BASED ON RBFN
Wang Jianbo;Yu Daren

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

APPLICATION OF MODEL-BASED FAULT DIAGNOSIS METHOD TO PROPULSION SYSTEM OF SPACECRAFT
Boyanheshig;Jiang Xingwei;Huang Wenhu

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

SIMULATION ON DYNAMIC CHARACTERISTICS OF TURBOJET ENGINE FOR MISSILES
Zhang Zhenjia;Yang Xinggen;Tong Shuhui

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