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UNSTEADY AERODYNAMIC FORCES AND FLUTTER ANALYSIS FOR A WING-AILERON-TAB CONFIGURATION
Yang Yongnian;Cheng Jingyun
1983, (1): 1-7.
PDF [ 334 K ]( 378 ) HTML
INDUCED ROLLING MOMENT ON WINGS OF A MISSILE WITH TILT-WINGS IN "X-X" CONFIGURATION AT SUPERSONIC SPEEDS
Yang Qiucheng;Kang Qingzhen
1983, (1): 8-15.
PDF [ 405 K ]( 488 ) HTML
EQUIVALENT ANGLE OF ATTACK FOR THE LIFTING PLANE WITH LINEAR CAMBER-TWIST AT LOW SPEEDS
Xu Daming
1983, (1): 16-21.
PDF [ 371 K ]( 330 ) HTML
THREE THEOREMS OF WEIGHT CHARACTERISTICS OF STATICALLY DETERMINATE AND INDETERMINATE STRUCTURES AND THEIR APPLICATION
Feng Yuansheng
1983, (1): 22-26.
PDF [ 303 K ]( 566 ) HTML
A CRACK GROWTH FATIGUE LIFE UNDER SPECTRUM LOADING
Yang Bingxian
1983, (1): 27-35.
PDF [ 902 K ]( 463 ) HTML
EXPERIMENTAL STUDY ON COMPRESSIVE PROPERTIES OF SHEETS AND PLATES AND SHAPES
Tong Jiaxian;Li Shunhe;Chen Shuqin
1983, (1): 36-42.
PDF [ 1311 K ]( 882 ) HTML
NONSYNCHRONOUS WHIRLS OF THE TURBINE ROTOR IN AEROJET ENGINES
1983, (1): 43-52.
PDF [ 505 K ]( 395 ) HTML
A NUMERICAL METHOD FOR WEAKENING SHOCK WAVE STRENGTH IN TRANSONIC CASCADE FLOW FIELDS
Lin Baozhen;Jiang Haoxin;Zhou Sheng
1983, (1): 53-61.
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AIRBORNE RADAR TRACKING SYSTEM BASED ON OPTIMAL FILTERING THEORY
Mao Shiyi
1983, (1): 62-72.
PDF [ 588 K ]( 385 ) HTML
A "Current" Statistical Model and Adaptive Tracking Algorithm for Maneuvering Targets
Zhou Hongren
1983, (1): 73-86.
PDF [ 734 K ]( 1459 ) HTML
RECOGNITION OF CUTTING STATES FOR DIFFICULT-TO-CUT MATERIALS——APPLICATION OF PATTERN RECOGNITION TECHNIQUE
Zhang Youzhen;Pan Liangxian;Liu Zhaofa;Wu Dianzong
1983, (1): 87-94.
PDF [ 436 K ]( 325 ) HTML
COMPLEX COMBINED CURVE DESIGN AND FITTING——A B-SPLINE MULTIPLE KNOT METHOD
Yao Aoqiu;Zhou Rurong;Ding Qiulin
1983, (1): 95-102.
PDF [ 437 K ]( 876 ) HTML
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