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OPTIMIZATION OF MULTI-ELEMENT AIRFOILS FOR MAXIMUM LIFTS IN SEPARATED FLOWS
Cao Jianfa;Chen Yanqing
1990, (8): 313-319.
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A MAXIMUM STRAIN MEMORY ELEMENT
Tao Baoqi;Zhang Weigong;Wang Ni;Chen Jie
1990, (8): 320-327.
AN EQUIVALENT CALCULATION OF LOAD SPECTRUMS
Meng Fanpei;Li Lingfang
1990, (8): 328-333.
THE INTERIM PREDICTION FOR AIRCRAFT NOISE
Tang Diyi;Li Wenlan;Qiao Weiyang;Liu Zhenxia
1990, (8): 334-342.
PREDICTIVE CONTROL OF OPTIMAL PATH TERRAIN FOLLOWING SYSTEM
Xiao Shunda;Chen Bengang
1990, (8): 343-347.
STUDY AND DESIGN OF EXECUTIVE SOFTWARE FOR DISTRIBUTED REAL-TIME CONTROL SYSTEMS
Wang Yi;Zhou Xingshe;Han Zhaoxuan
1990, (8): 348-353.
A MAXIMUM LIKELIHOOD METHOD FOR FLIGHT TEST DATA COMPATIBILITY CHECK
Shi Zhongke
1990, (8): 354-360.
NUMERICAL SIMULATION OF THE HEATING PROCESS FOR DISK FORGING BILLET OF ALLOY GH169
Tang Hao;Lu Xinli;Luo Zijian
1990, (8): 361-368.
SHORT FATIGUE CRACK GROWTH BEHAVIOR IN 8090 ALUMINIUM-LITHIUM ALLOY
Chen Zheng
1990, (8): 369-374.
DISCUSSION ON THE SPECIFICATION OF CALIBRATION SYSTEM FOR A STRAIN GAGE BALANCE
Ouyang Wan
1990, (8): 375-378.
CONTACT STRESS ANALYSIS OF COMPOSITE LAMINATE WITH PIN-LOADED HOLES
Chen Haoran;Xi Zhichen
1990, (8): 379-382.
ON SMALL FATIGUE CRACKS
Guo Wanlin;Fu Xiangjiong
1990, (8): 383-386.
KEY PROBLEMS IN SOFTWARE DESIGN OF JBYQC
He Linshu
1990, (8): 387-388.
A METHOD OF TWO-DIMENSIONAL PARTITION FOR DESIGNING A LARGE-SCALE PROJECT NETWORK
Ning Xuanxi;Ma Zifeng
1990, (8): 389-392.
A METHOD OF DEVELOPING LOAD SPECTRUM FOR A FIGHTER AIRCRAFT
Wang Zhi;Li Shuwen;Liu Wenqi
1990, (8): 393-395.
FLOWFIELD COMPUTATION OF 2-C-D NOZZLE
Chen Baisong;Wu Da
1990, (8): 396-399.
CORROSION FATIGUE CRACK GROWTH OF 30CrMnSiNi2A STEEL IN AIRPLANE ENVIRONMENTS
Niu Kangmin;Chen Meiying;Ju Xuening
1990, (8): 400-404.
LASER COATING OF TI6A14V
Li Hualun;Molian P.A.
1990, (8): 405-409.
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