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AN APPROXIMATE ANALYTICAL METHOD FOR VORTEX-LIFT AND CENTRE OE PRESSURE ON THE SLENDER WING
Yin Xieyuan
1980, (1): 1-6.
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A PENALTY FUNCTION METHOD FOR STRUCTURAL OPTIMUM DESIGN WITH AEROELASTIC CONSTRAINTS
Wang Xianxin
1980, (1): 7-15.
AN AERONAUTICAL STRUCTURAL ANALYSIS SYSTEM FOR STATIC ANALYSIS（HAJIF-I）
Feng Zhongyue
1980, (1): 16-26.
A FAMILY OF TAPERED BEAM CONFORMING ELEMENTS AND ITS APPLICATION TO BEAM NATURAL VIBRATION ANALYSIS
Zhu Dechao
1980, (1): 27-41.
CALCULATION OF INTERNAL AND EXTERNAL FLOW FIELD AND COWL PRESSURE DRAG IN THE SUPERSONIC AXISYMMETRIC NOSE INLETS
Zhou Weimin;Xu Suiwen
1980, (1): 42-53.
THE METHOD FOR CALCULATING THE FUEL CONCENTRATION FIELD IN THE DOWNSTREAM POSITIONS OF THE PRESSURE JET ATOMIZER IN THE HIGH TEMPERATURE GAS-STREAM
Fu Weibiao
1980, (1): 54-52.
A VEHICLE ATTITUDE CONTROL SYSTEM FORMING THE ERROR SIGNAL BY WAY OF THE OPTIMAL ROTATION AXIS
Dai Zongli;Shi Ruohua;Bi Dachuan
1980, (1): 63-73.
ON THE APPLICATION OF SELF-ADAPTIVE FLIGHT CONTROL SYSTEM BASED ON ENERGY BALANCE THEORY
Li Lichun
1980, (1): 74-81.
DIGITAL FILTER NETWORK DESIGN BY USING OBSERVERS
Zhang Fuzhong
1980, (1): 82-91.
ON THE DERIVATION OF BEZIER'S BASIC FUNCTIONS
Shi Fazhong;Han Daokang
1980, (1): 92-98.
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