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AERODYNAMIC CHARACTERISTICS OF MANEUVERING FLAPS
Fang Baorui;Hu Bingke;Wang Huixuan;Zhang Yulian
1981, (3): 1-13.
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NUMERICAL CALCULATION OF LIFT, MOMENT COEFFICIENT AND DYNAMIC STABILITY DERIVATIVES ON SIDESLIPPING WINGS IN UNSTEADY SUPERSONIC FLOWS
Zhang Guofu
1981, (3): 14-22.
NUMERICAL COMPUTATION OF UNSTEADY SUBSONIC AERODYNAMIC FORCES ON WING-BODY-TAIL EXPOSED TO TRAVELLING GUST
Wen Gongbi;Sun Zhongshu
1981, (3): 23-30.
CALCULATION OF STRESS INTENSITY FACTORS WITH HYBRID STRESS ELEMENTS AND ISOPARAMETRIC ELEMENTS
He Jifan;Chang Liangming;Gao Zhanmin;Li Zhousheng;Sun Duxin
1981, (3): 31-41.
AN ATTEMPT TO DERIVE A VARYING THICKNESS PLATE ELEMENT FROM HYBRID DISPLACEMENT METHOD
Zhang Gongxing;Yu Junjiang
1981, (3): 42-49.
ON THE VIBRATION OF THE FIBER REINFORCED LAMINATED PLATES
Zhang Jidong
1981, (3): 50-54.
A DYNAMIC REDUCING ITERATIVE METHOD FOR SOLVING LARGE GENERALIZED EIGENVALUE PROBLEMS
Zhang Wen;Hou Zhikun
1981, (3): 55-61.
STATISTICAL ESTIMATION OF LIQUID PROPELLANT ROCKET ENGINE PARAMETERS
He Guowei
1981, (3): 62-66.
NUMERICAL TESTS OF THREE-DIMENSIONAL FLOW IN A TRANSONIC TURBINE
Zhang Yaoke;Gong Zengjin;Shen Mengyu
1981, (3): 67-76.
THE EFFECT OF THE STATOR WITH UNEQUAL PITCH CASCADES ON THE COMPRESSOR BLADE VIBRATION
Li Zuochang
1981, (3): 77-83.
THE SIMULATION STUDY ON A REDUNDANT FLIGHT CONTROL SYSTEM
Xue Dajiong
1981, (3): 84-93.
A RAPIDLY RECURSIVE METHOD FOR THE B-SPLINES
Yuan Qisun
1981, (3): 94-103.
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