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FLUX-SPLITTING IMPLICIT FINITE VOLUME METHOD FOR THE CALCULATION OF THE SUPERSONIC FLOW WITH STRONG INTERACTION OF A JET
Wang Zhenghua;Wang Chengyao
1996, (1): 1-8.
PDF [ 411 K ]( 492 ) HTML
AN ADAPTIVE-GRID ALGORITHM FOR COMPUTING HIGH SPEED COMPLEX FLOWS
Li Chunxuan;Yang Hongwei
1996, (1): 9-17.
PDF [ 346 K ]( 683 ) HTML
EXPERIMENTAL INVESTIGATIONS ON DIMENSIONLESS TEM PERATURE DIFFERENCE RATIO η AND θ OF MAT-WALL COOLING STRUCTURE
He Liming;Li Changlin;Wu Erping
1996, (1): 18-23.
PDF [ 265 K ]( 533 ) HTML
FAULTY ANALYSIS OF PRESSURE BELLOWS FOR PROPELLER REGULATING SYSTEM
Ma Rui;Li Wei;Li Chunhua
1996, (1): 24-29.
PDF [ 311 K ]( 393 ) HTML
REPETITIVE MOTION CONTROL OF SPACE ROBOT SYSTEM WITH A LEAST USE OF ATTITUDE CONTROL FUEL
Ma Baoli;Huo Wei;Gao Weibing
1996, (1): 30-35.
PDF [ 310 K ]( 460 ) HTML
ROBUST CONTROLLER DESIGN FOR SELF-REPAIRING FLIGHT CONTROL SYSTEM
Qiu Xiaohong;Gao Jinyuan;Zhang Linchang
1996, (1): 36-41.
PDF [ 307 K ]( 500 ) HTML
A PARALLEL EXTENDED KALMAN FILTER FOR SPACECRAFT RELATIVE MOTION ESTIMATION
Chen Genshe;Wen Chuanyuan;Chen Xinhai
1996, (1): 42-50.
PDF [ 398 K ]( 614 ) HTML
UNDERCOOLING AND STRUCTURE OF Al-4.5%Cu Alloy
Jian Zengun;Yang Gencang;zhou Yaohe
1996, (1): 51-54.
PDF [ 197 K ]( 853 ) HTML
PREPARATION AND PROPERTIES OF ITO TRANSPARENT CONDUCTING FILMS
Yue Xihua;Zhao Yi;Zhang Weijia
1996, (1): 55-61.
PDF [ 273 K ]( 1048 ) HTML
RESEARCH ON THE TOOL COATED BY Ti(Y)N AND THE INTERFACIAL STATUS OF COATING-SUBSTRATE
Feng Zheng;Liu Dejun
1996, (1): 62-67.
PDF [ 280 K ]( 433 ) HTML
GENERAL MATHEMATIC SIMULATION METHOD FOR SYNCHRONOUS GENERATOR-SEMICONDUCTOR RECTIFIER SYSTEMS
Xie Shaojun;Yan Yangguang
1996, (1): 68-74.
PDF [ 282 K ]( 876 ) HTML
EFFECT OF DIFFERENT PROCESSES ON THE MECHANICAL PROPERTIES AND MICROSTRUCTURES OF A NiAl-30Fe-Y ALLOY
Wang Shuhe;Guo Jianting;Lai Wanhui;He Lianlong
1996, (1): 75-82.
PDF [ 350 K ]( 584 ) HTML
NUMERICAL SIMULATIONS OF INTERNAL FLOW CHARACTERISTICS IN TWO-DIMENSIONAL NOZZLES WITH THRUST VECTORING
Yang Hongwei;Li Chunxuan
1996, (1): 83-85.
PDF [ 229 K ]( 587 ) HTML
COMPUTATION OF COMPRESSIBLE FLOW PAST SLENDER WING-BODY USING FULL-POTENTIAL EQUATION
Huang Mingke
1996, (1): 86-89.
PDF [ 290 K ]( 513 ) HTML
3-D NUMERICAL SIMULATION OF UNDERWATER EXPLOSION BUBBLES
Lu Chuanjing
1996, (1): 90-93.
PDF [ 179 K ]( 1029 ) HTML
STEADY STATE ANALYSIS FOR SERIES OUTPUT DC/DC RESONANT CONVERTER
Ding Daohong;Yang Dongping
1996, (1): 94-98.
PDF [ 177 K ]( 567 ) HTML
THE RESISTANCE FUZZY OBSERVER OF AC SERVO SYSTEM
Hu Yuwen;Tang Lixin
1996, (1): 99-104.
PDF [ 304 K ]( 448 ) HTML
ROBUST STABILIZATION OF NONLINEAR UNCERTAIN SYSTEMS
Fei Shumin;Gao Weibing
1996, (1): 105-109.
PDF [ 277 K ]( 466 ) HTML
ROBUST FAULT-TOLERANT CONTROL AND DESIGN FOR UNCERTAIN LINEAR SYSTEMS
Wang Zidong Sun Xiang;Sun Jinsheng;Wang Zhiquan
1996, (1): 110-113.
PDF [ 250 K ]( 573 ) HTML
ROBUST PI DECOUPLING DESIGN OF HELICOPTER FLIGHT CONTROL SYSTEM
Wang Yandong;Cheng Peng
1996, (1): 114-118.
PDF [ 274 K ]( 678 ) HTML
STUDY ON THE BEST PROFILE MODIFICATION OF HIGH-SPEED SPUR GEARS WITH HIGH-CONTACT-RATIO
Wang Sanmin;Ji Minggang
1996, (1): 119-122.
PDF [ 165 K ]( 825 ) HTML
MICROSTRUCTURE OF THE HOLE EXPANSION STRENGTHENED LAYER OF HIGH TEMPERATURE ALLOY GH169
Song Deyu;Luo Zhiping;Yang Yurong;Zhang Shaoqing
1996, (1): 123-126.
PDF [ 261 K ]( 512 ) HTML
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