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RELAXATION COMPUTATION OF TRANSONIC FLOWS AROUND WINGS WITH BLUNT LEADING-EDGE AND DISCUSSION ON ITS STABILITY AND CONVERGENCE
Zheng Yuwen;Luo Shijun
1982, (3): 1-14.
PDF [ 638 K ]( 411 ) HTML
DETERMINATION OF AERODYNAMIC COEFFICIENTS FOR A RE-ENTRY BODY BY MEANS OF AN EXTENDED KALMAN FILTER
Jiang Quanwei;Xu Jinzhi;Zhou Shuying
1982, (3): 15-24.
PDF [ 493 K ]( 673 ) HTML
A PROGRAM SYSTEM FOR DYNAMIC ANALYSIS OF AERONAUTICAL STRUCTURES（HAJIF-Ⅱ）
Guan De
1982, (3): 25-32.
PDF [ 466 K ]( 320 ) HTML
SYSTEM IDENTIFICATION AND AIRCRAFT FLUTTER
Zhang Lingmi
1982, (3): 33-41.
PDF [ 507 K ]( 299 ) HTML
APPLICATION OF MULTIPLE DYNAMIC ABSORBERS TO REDUCING THE VIBRATION LEVEL OF A COMPLEX CANTILEVER STRUCTURE
Tian Qianli
1982, (3): 42-49.
PDF [ 437 K ]( 310 ) HTML
A SPECTRAL APPROACH FOR ANALYZING THE VIBRATION OF A PERIODIC STRUCTURE WITH RANDOM PARAMETERS
Huang Wenhu
1982, (3): 50-62.
PDF [ 645 K ]( 347 ) HTML
A NEW METHOD OF FINITE ELEMENT STRUCTURE DISCRETIZATION
Liang Guowei
1982, (3): 63-69.
PDF [ 423 K ]( 292 ) HTML
COMPUTER RESEARCH ON DYNAMIC CHARACTERISTICS OF A SYNCHRO GENERATOR
Qian Zhenxiong;Xu Qiaobao
1982, (3): 70-80.
PDF [ 599 K ]( 280 ) HTML
ELECTRONIC CIRCUIT ANALYSIS LANGUAGE（ECAL）
Chen Chenghang
1982, (3): 81-87.
PDF [ 406 K ]( 232 ) HTML
AN EXPERIMENTAL INTERACTIVE COMPUTER GRAPHICS SYSTEM FOR FREE-FORM SURFACE DESIGN
Zheng Huiling;Wang Zhisheng;Lu Hongjia;He Tianbao
1982, (3): 88-96.
PDF [ 461 K ]( 273 ) HTML
BEZIER'S PLOTTING THEOREM AND GEOMETRICAL CHARACTERISTICS OF CUBIC BEZIER CURVES
Shi Fazhong;Wu Junheng
1982, (3): 97-104.
PDF [ 409 K ]( 521 ) HTML
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