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APPLIED SAFETY FACTOR IN DESIGN OF COMPOSITE MATERIAL STRUCTURES
Zheng Jinyong
1988, (1): 1-10.
PDF [ 744 K ]( 524 ) HTML
APPLICATION OF EFFICIENT ITERATION SCHEME AF2 TO COMPUTATIONS OF TRANSONIC FULL-POTENTIAL FLOWS OVER WING-BODY CONBINATIONS
Huang Mingke
1988, (1): 11-18.
PDF [ 498 K ]( 317 ) HTML
NUMERICAL CALCULATION OF A CLASS OF OPTIMAL FLIGHT TRAJECTORIES
Wang Peide;Cui Taorui;Hou Ming
1988, (1): 19-25.
PDF [ 459 K ]( 763 ) HTML
THE MODELLING TECHNIQUE OF THE FLIGHT SYSTEM IN FLIGHT SIMULATOR
Zhao Zhenyan
1988, (1): 26-33.
PDF [ 626 K ]( 1312 ) HTML
STRESSES ANALYSIS AROUND A PIN-LOADED HOLE IN COMPOSITE LAMINATES BY AN ANALYTIC-NUMERICAL METHOD
Shan Huizu;Yang Naiwen
1988, (1): 34-40.
PDF [ 416 K ]( 368 ) HTML
SOME ASPECTS OF THE RELIABILITY ANALYSIS OF AIRCRAFT STRUCTURES
Zhu Depei;Lin Fujia
1988, (1): 41-49.
PDF [ 560 K ]( 301 ) HTML
A NEW TWO STAGE RECURSIVE ESTIMATION FOR ARMAX PROCESSES
Lu Boying;Wan Guolong
1988, (1): 50-59.
PDF [ 518 K ]( 1678 ) HTML
A CONTINUOUS MINIMAL ORDER SINGULAR FILTER
Hu Shousong;Xu Jinfa
1988, (1): 60-68.
PDF [ 493 K ]( 382 ) HTML
EFFECT OF +G STRESS AT DIFFERENT SEAT BACK ANGLES ON HUMAN OPERATOR TRACKING PERFORMANCE
Xie Baosheng;Qi Zhangnian;Xu Zhenyong;Liu Guanyuan
1988, (1): 69-74.
PDF [ 1756 K ]( 413 ) HTML
PDF [ 1756 K ]( 403 ) HTML
EXPERIMENTAL INVESTIGATIONS ON THE DAMAGE GROWTH OF GRAPHITE/EPOXY LAMINATES WITH A HOLE UNDER TENSION-COMPRESSION FATIGUE
Zhao Shixi;R.Prinz;H.C.Goetting
1988, (1): 75-83.
PDF [ 1429 K ]( 831 ) HTML
EXPERIMENTAL INVESTIGATION ON RIGID HOLLOW HEMISPHERICAL PARACHUTE MODEL IN ACCELERATING AND STEADY FLOW
Lian Qixiang;Zhou Minxuan
1988, (1): 84-90.
PDF [ 1429 K ]( 327 ) HTML
LINEAR DYNAMICS OF SUPERSONIC INLET
Guan Yanshen;Yang Xin;Ku Zuo
1988, (1): 91-96.
PDF [ 371 K ]( 326 ) HTML
A SIMPLIFIED METHOD FOR CALCULATING EIGENVECTOR DERIVATIVES
Chen Jifeng
1988, (1): 97-102.
PDF [ 361 K ]( 925 ) HTML
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