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SOLIDIFICATION OF HIGHLY UNDERCOOLED METALLIC MELTS
Wei Bingbo;Yang Gencang;Zhou Yaohe
1991, (5): 213-220.
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TRANSONIC AIRFOIL ANALYSIS BASED ON THE INTERACTION OF EULER AND INTEGRAL BOUNDARY-LAYER EQUATION
Cai Hanlong;Li Feng
1991, (5): 221-227.
THE EARLY DEVELOPMENT OF THE FLOW AROUND AN IMPULSIVELY STARTED CIRCULAR CYLINDER
Sun Mao;Luo Jiang
1991, (5): 228-233.
AN AF3 ALGORITHM FOR THE CALCULATION OF TRANSONIC NONCONSERVATIVE FULL POTENTIAL FLOWS OVER WINGS OR WING/BODY COMBINATIONS
Chen Hongquan;Huang Mingke
1991, (5): 234-240.
SOME PROBLEMS ABOUT THE ATMOSPHERIC TURBULENCE SPECTRUM AND AIRCRAFTRESPONSE
Xu Ke;Xiao Yelun;Zhang Guilian
1991, (5): 241-248.
TWO-LEVEL STRUCTURE OPTIMIZATION METHOD BASED ON ADAPTIVE MULTI-POINT CONSTRAINT APPROACHING
Huang Hai;Xia Renwei
1991, (5): 249-255.
ANALYSIS OF TRANSIENT TEMPERATURE AND THERMAL STRESS FIELD IN LAMINATED COMPOSITE SHELLS OF REVOLUTION
Chen Haoran;Xi Zhichen;Li Hongwei;Cheng Wanzhi;Sun Yanbo
1991, (5): 256-263.
A MODEL FOR RELIABILITY ASSESSMENT OF STRUCTURES
Fu Huimin;Gao Zhentong
1991, (5): 264-271.
A NUMERICAL COMPUTATION OF HEAT TRANSFER ON CURVED WALL WITH FILM COOLING
Jiang Tao;Liu Songling
1991, (5): 272-278.
THE MODEL REFERENCE FAULT TOLERANT CONTROL IN AIRCRAFT
Hu Shousong;Cheng Jiong
1991, (5): 279-286.
DISCUSSION ON THE INTEGRATION APPROACHES AND NAVIGATION PERFORMANCE OF INTEGRATED GPS/INERTIAL NAVIGATION SYSTEMS
Yu Jixiang;Zhang Gengsheng
1991, (5): 287-293.
BISTATIC RADAR CROSS SECTION FOR REFLECTOR ANTENNAS
Deng Shuhui;Ruan Yingzheng
1991, (5): 294-302.
CREEP-FATIGUE LIFE PREDICTION UNDER THE CONDITION OF TENSION-TENSION STRESS
Su Hangshfeng;He Jinrui
1991, (5): 303-309.
ON THE SUPERLATTICE PHASE IN AI-Li ALLOY
Jin Yan;Li Chunzhi;Yan Minggao;Ye Hengqaing
1991, (5): 310-315.
DERIVATION OF THE TWO DIMENSIONAL TRANSONIC TIME LINERIZED INTEGRAL EQUATION
Su Jichao;Wu Liyi
1991, (5): 316-320.
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