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A SUPER-ELEMENT METHOD FOR VIBRATION CHARACTERISTIC ANALYSIS OF STRUCTURES
Chen Guo-ping;Zhu De-mao
1992, (9): 465-471.
PDF [ 382 K ]( 981 ) HTML
STRUCTURAL DYNAMIC MODEL UPDATING BASED ON SENSITIVITY ANALYSIS
Qi Pi-qian;Zhang Ling-xia
1992, (9): 472-475.
PDF [ 259 K ]( 689 ) HTML
DETERMINATION OF THE PHYSICAL LOCATION OF MODEL ERRORS
Qian Guan-liang;Gu Song-nian
1992, (9): 476-479.
PDF [ 229 K ]( 379 ) HTML
PERTURBATION ANALYSIS OF THE COMPLEX EIGENSOLUTIONS FOR DAMPED VIBRATION SYSTEM
Sun Jiu-hou;Zhu De-man
1992, (9): 480-483.
PDF [ 227 K ]( 441 ) HTML
SECTIONAL WARPING CORRECTIVE THEORY FOR COMPOSITE LAMINATED STRUCTURES
Huang Chuan-yao;Zhu De-chao
1992, (9): 484-490.
PDF [ 405 K ]( 460 ) HTML
A HIGH-ORDER THEORY AND FINITE ELEMENT MODEL OF COMPOSITE LAMINATED PLATES AND DELAMINATED PLATES
Hu Lie;Jiang Jie-sheng
1992, (9): 491-497.
PDF [ 347 K ]( 471 ) HTML
TRANSIENT RESPONSE OF LAYERED COMPOSITE PLATES
Ding Xi-hong;Zhou Li;Gu Hui-zhi
1992, (9): 498-502.
PDF [ 286 K ]( 577 ) HTML
A NEW HIGH-ORDER VIBRATION THEORY AND FINITE ELE-MENT MODEL OF COMPOSITE LAMINATED PLATES
1992, (9): 503-506.
PDF [ 237 K ]( 478 ) HTML
WHEEL SHIMMY ANALYSIS FOR MAIN LANDING GEAR OF AIRCRAFT
Zhu De-pei
1992, (9): 507-509.
PDF [ 176 K ]( 659 ) HTML
ANALYSIS OF STRUCTURAL DYNAMIC RESPONSE FOR AIRCRAFT OPERATING IN THE ENVIRONMENT OF NUCLEAR EXPLOSION SHOCK WAVES
Zhang Sen-lin
1992, (9): 510-515.
PDF [ 343 K ]( 526 ) HTML
A NEW APPROACH TO ANALYSING THE VIBRATION CHARACTERISTICS OF COMPOSITE BLADES
Wang Xing-wei;Cai Hui-lian;Wang Shou-mei
1992, (9): 516-521.
PDF [ 310 K ]( 551 ) HTML
ROBUST CONTROLLER DESIGN FOR STRUCTURAL VIBRATION BASED ON TOLERANCE CONTROL STRATEGY
Chen Wei-dong;Gu Zhong-quan
1992, (9): 522-527.
PDF [ 371 K ]( 338 ) HTML
HIGHER-ORDER UPDATES AND SENSITIVITY ANALYSIS FOR DYNAMIC RESPONSES IN STRUCTURAL OPTIMIZATION DESIGN
Kong Jian-hua;Ge Zu-de;Yao Oi-hang
1992, (9): 528-533.
PDF [ 362 K ]( 432 ) HTML
STRUCTURAL DYNAMIC DESIGN OF MULTIFREQUENCY OPTIMAL AND FREQUENCY RESPONSE OPTIMAL
Shi Rong-ming;Zhu De-mao
1992, (9): 534-537.
PDF [ 238 K ]( 468 ) HTML
BIRD IMPACT DYNAMIC RESPONSE ANALYSIS FOR AIRCRAFT ARC WINDSHIELD
Zhang Zhi-lin;Zhang Qi-qiao;Li Ming-xing
1992, (9): 538-542.
PDF [ 288 K ]( 518 ) HTML
INVESTIGATION OF CABIN NOISE REDUCTION IN THE Yl2
Yao Qi-hang;Huang Wen-chao;Ma Xiao-jun
1992, (9): 543-547.
PDF [ 302 K ]( 806 ) HTML
A SHORT INTRODUCTION TO THE LINEAR FLUID-SOLID INTERACTION DYNAMIC ANALYSIS PROGRAM FSIAP 92
Xing Jing-tang
1992, (9): 548-551.
PDF [ 253 K ]( 459 ) HTML
TRANSITION OF FLUTTER MODE OF TWO-DIMENSIONAL WING WITH EXTERNAL STORE
Yang Zhi-chun;Zhao Ling-cheng
1992, (9): 552-554.
PDF [ 206 K ]( 565 ) HTML
LIMIT CYCLE OSCILLATION OF A FLUTTERING PLATE
Ye Wei-liang
1992, (9): 555-559.
PDF [ 272 K ]( 525 ) HTML
EFFECTS OF THE PYLON PITCHING STIFFNESS ON WING-STORE FLUTTER
Wang Li-jun;Zhao Ling-cheng
1992, (9): 560-563.
PDF [ 244 K ]( 394 ) HTML
THE INVESTIGATION ON VIBRATION CHARACTERISTICS OF ALL MOVABLE STABILIZER OF AN AIRCRAFT
Xiao Ying-ben;Zhou Da-quan(Box-0;Xi'an;Xi'an;00)
1992, (9): 564-566.
PDF [ 214 K ]( 538 ) HTML
THE DESIGN OF SHOCK-ABSORPTION INSFALLATION FOR AERO-ENGINES
Gong Qing-xiang
1992, (9): 566-567.
PDF [ 139 K ]( 635 ) HTML
RESEARCH AND MANUFACTURE OF THE COMPREHENSIVE ENVIRONMENT TESTING BOX
Wang Shao-liang;Guo Gui-zhi
1992, (9): 567-568.
PDF [ 145 K ]( 415 ) HTML
ELECTROSIMULATION TECHNOLOGY OF STRUCTURAL NON-LINEARITY
Lu Wen-ming
1992, (9): 568-569.
PDF [ 140 K ]( 335 ) HTML
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