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OSCILLATORY SUBSONIC POTENTIAL FLOWS AROUND THREE-DIMENSIONAL BODIES AND ITS APPLICATION TO THE CALCULATION OF DYNAMIC STABILITY DERIVATIVES OF THE AIRCRAFT
Liu Qiangang;Wu Changlin;Jian Zheng
1981, (2): 1-9.
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AN INTERPOLATION MIXED DIFFERENTIAL METHOD FOR TRANSONIC LARGE DISTURBED SYMMETRICAL POTENTIAI FLOW AROUND AIRFOIL
Ling Heyao
1981, (2): 10-17.
THE CALCULATION OF LIFT AND DRAG CHARACTERISTICS OF SUBSONIC WINGS WITH WINGLETS
Zhou Renliang
1981, (2): 18-25.
A NEW MODEL FOR PREDICTING OVERLOAD RETARDATION EFFECT IN FATIGUE CRACK PROPAGATION
He Qingzhi
1981, (2): 26-34.
J-INTEGRAL EXPERIMENTAL CALIBRATION OF SHEET SPECIMENS WITH SINGLE EDGE NOTCH
Luo Ligeng;Chen Xianxi;Cat Qigung;Zheng Minzhung
1981, (2): 35-41.
ON THE DESIGN OF TRANSONIC TURBINE CASCADE BY HODOGRAPH METHOD
Ling Zhiguang;Xin Shaokong;Zhu Shican
1981, (2): 42-53.
THREE-DIMENSIONAL STRESS ANALYSIS FOR A SHROUDED AIR-COOLED TURBINE BLADE
Shung Changbing;Xiao Junxiang
1981, (2): 54-67.
A STUDY OF THE METHODS FOR MEASURING RADAR'S ECCM PERFORMANCE
Li Nengjing
1981, (2): 68-84.
THE OPTIMUM DESIGN OF NON-MOMENT LAMINATED COMPOSITE PLATE -According to static failure strength condition
Ma Zukang
1981, (2): 93-102.
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