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FRETTING DAMAGE IN AIRCRAFT INDUSTRY AND THE GENERAL SITUATION OF RESEARCH
Li Dongzi;Wang Buying
1987, (11): 535-542.
PDF [ 1729 K ]( 564 ) HTML
CALCULATION OF TRANSONIC FLOWS AROUND AEROFOILS BY INTEGRAL EQUATION METHOD
Su Jichao;Wu Liyi
1987, (11): 543-552.
PDF [ 502 K ]( 375 ) HTML
WING BOUNDARY LAYER CALCULATION AND IT'S APPLICATION TO THE AIRCRAFT DESIGN
Bao Hanling
1987, (11): 553-560.
PDF [ 438 K ]( 573 ) HTML
A STUDY OF THE GLOBAL. STABILITY OF HIGH PERFORMANCE AIRCRAFTS AT HIGH ANGLE-OF-ATTACK
Gao Hao;Zhou Ziqiang
1987, (11): 561-571.
PDF [ 586 K ]( 489 ) HTML
ON FATIGUE CRACK GROWTH UNDER MIXED MODE CYCLIC LOADING
Dai Yi;Zheng Guanghua;Hong Qilin
1987, (11): 572-578.
PDF [ 588 K ]( 402 ) HTML
A STUDY OF DIFFERENTIAL GAME OPTIMAL GUIDANCE LAWS FOR AIR-TO-AIR MISSILES
Hou Mingshan
1987, (11): 579-586.
PDF [ 449 K ]( 468 ) HTML
A RESEARCH OF NON-LINEAR OBSERVERS FOR LATERAL MOTION OF AIRCRAFTS
Wang Zangxue
1987, (11): 587-596.
PDF [ 548 K ]( 301 ) HTML
ON LOCAL STATE FEEDBACK AND STABILITY DOMAIN ESTIMATION OF NONLINEAR LARGE SCALE SYSTEMS
Yu Runyi;Gao Weibing
1987, (11): 597-604.
PDF [ 434 K ]( 304 ) HTML
A SIMULATION STUDY OF CRYSTAL FORMATION IN LIQUID ZONE DURING SOLIDIFICATION
Jie Wanqi;Zhou Yaohe
1987, (11): 605-612.
PDF [ 955 K ]( 1282 ) HTML
STRESS AND STABILITY ANALYSIS FOR COMPOSITE SHELL STRUCTURES
Cai Yiping;Li Li;Xue Kexing
1987, (11): 613-618.
PDF [ 363 K ]( 927 ) HTML
IMPROVEMENTS ON MOTYCKA METHOD OF PREDICTING MAXIMUM EXPECTED INSTANTANEOUS INLET FLOW DISTORTION
Liang Dewang;Zhang Shiying
1987, (11): 619-622.
PDF [ 237 K ]( 283 ) HTML
PULSE TECHNIQUE FOR MEASURING THE VIBRATION OF ROTOR BLADES
Zhang Yisong;Yi Liyan
1987, (11): 623-627.
PDF [ 276 K ]( 366 ) HTML
PLY ANGLE EFFECT ON CRITICAL VALUES OF A BECK-TYPE LAMINATED COLUMN
Xiong Yusxi;Wang Junkuei
1987, (11): 628-631.
PDF [ 218 K ]( 384 ) HTML
THE FAILURE LIFE UNDER COMBINED CREEP AND FATIGUE FOR GH36
Tian Changsheng;Qiao Shengru;Tao Yie;Rong Yichao
1987, (11): 632-636.
PDF [ 768 K ]( 277 ) HTML
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