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A FINITE ELEMENT METHOD FOR INTEGRAL REPRESENTATIONS OFINAVIER-STOKES EQUATION
Hua Jun
1987, (4): 121-126.
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ANALYSIS AND CALCULATION OF FIGHTER GUN RECOIL FORCE
Luo Yuanxiang;Liu Yipu;Xue Kezong
1987, (4): 127-135.
PDF [ 383 K ]( 379 ) HTML
SMOOTH QUADRATIC INTERPOLATION OVER A CONVEX 3D TRIANGULATION
Jiang Shoushan;Yang Pengji
1987, (4): 136-139.
PDF [ 642 K ]( 375 ) HTML
CLOSE FORM SOLUTION FOR PREDICTION OF CRACK PROPAGATION LIFE OF STRUCTURE MEMBER AND ITS APPLICATION TO LANDING GEARS
Zhang Xing;Wu Baoxin;Wei Hueizhu
1987, (4): 140-146.
PDF [ 567 K ]( 349 ) HTML
FINITE ELEMENT ANALYSIS FOR COMPOSITE HONEYCOMB SANDWICH AND/OR METAL STRUCTURE
Liu Xiashi
1987, (4): 147-156.
PDF [ 421 K ]( 329 ) HTML
DEVELOPMENT OF FUEL PUMP-MOTOR ROTATIONAL SPEED CONTROL SYSTEM
Chen Zheng;Zhu Rongchu;Zeng Junying
1987, (4): 157-164.
PDF [ 529 K ]( 389 ) HTML
EFFECTS OF SWIRLING AIRFLOW AND DIVERGENCE ANGLE OF AIRBLAST ATOMIZER ON ATOMIZATION PERFORMANCE
Zhao Qishou;Lin Lijun;Yuan Quanchao
1987, (4): 165-170.
PDF [ 416 K ]( 523 ) HTML
DESIGN OF FLIGHT CONTROL SYSTEM WITH MANEUVER ENHANCEMENT AND GUST ALLEVIATION
Yang Yidong;Wang Jianping
1987, (4): 171-178.
PDF [ 311 K ]( 484 ) HTML
A COMPUTATIONAL METHOD. FOR STABILITY AND MANEUVERABILITY OF HELICOPTER
Xin Zhiming;Tian Yongcheng;You Zhongxiao
1987, (4): 179-185.
PDF [ 458 K ]( 345 ) HTML
A MODEL FOR PREDICTION OF FATIGUE CRACK GROWTH UNDER VARIABLE AMPLITUDE LOADING
Wang Zhizhi;Mie Xuezhou
1987, (4): 186-190.
PDF [ 435 K ]( 315 ) HTML
A UNIVERSALLY APPLICABLE FATIGUECRACK-GROWTH-RATE DECRIPTION
Wang Yonglian;Wu Yongduan
1987, (4): 191-197.
PDF [ 311 K ]( 979 ) HTML
EFFECTS OF REDUNDANCY CONFIGURATION AND ITS MANAGEMENT MODE ON THE RELIABILITY OF FLIGHT CONTROL SYSTEM
Li Lichun
1987, (4): 198-203.
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CROSS-CHORD METHOD——AN EASY APPROACH TO BEST FITTING QUADRATIC POLYNOMIALS TO DATA
Sun Dehui
1987, (4): 204-208.
ON THE CALCULATION OF FLOW STRESS OF MATERILA IN PRECISION BLADEFORGING
Zhu Jin;Zhang Zhiwen
1987, (4): 209-213.
PDF [ 1009 K ]( 336 ) HTML
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