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STATE-SPACE AEROELASTIC MODELING AND ITS APPLICATION IN FLUTTER CALCULATION
Lu Shuquan
1982, (4): 1-11.
PDF [ 564 K ]( 381 ) HTML
STUDY ON LONGITUDINAL DYNAMIC CHARACTERISTICS OF PILOT-AIRPLANE SYSTEM--APPROACH TO THE METHOD FOR STUDYINGPIO PROBLEM
Chen Tingnan;Li Chunzhu
1982, (4): 12-20.
PDF [ 463 K ]( 277 ) HTML
STATISTICAL DETERMINATION OF A FLAW DETECTION PROBABILITY CURVE
Lin Fujia;Huang Yushan
1982, (4): 21-27.
PDF [ 411 K ]( 982 ) HTML
MULTI-LEVEL SUBSTRUCTURAL ANALYSIS IN MODAL SYNTHESIS--TWO IMPROVED SUBSTRUCTURAL ASSEMBLING TECHNIQUES
Liu Guoguang;Li Junjie;Zhang Dewen penned
1982, (4): 28-35.
PDF [ 477 K ]( 460 ) HTML
9-NODE QUADRILATERAL ISOPARAMETRIC ELEMENT
Wu Yongli
1982, (4): 36-40.
PDF [ 284 K ]( 1506 ) HTML
APPLICATION OF LASER HOLOGRAPHIC INTERFEROMETRY TO VIBRATION ANALYSIS OF AEROCRAFT BEAM STRUCTURE MODEL
Jin Guanchang;Wang Shengxiao;Chen Guobing;Shen Peiqing
1982, (4): 41-46.
PDF [ 925 K ]( 484 ) HTML
ON EXPERIMENTAL METHODS FOR DETERMINING CRITICAL SPEEDS
Yan Litang;Li Qihan
1982, (4): 47-52.
PDF [ 388 K ]( 1648 ) HTML
AN AZIMUTH RATE INERTIAL NAVIGATION SYSTEM
Ren Sicong;Zhao Yongkang
1982, (4): 53-60.
PDF [ 459 K ]( 316 ) HTML
THREE-DIMENSIONAL ELASTOPLASTIC FINITE ELEMENT ANALYSIS
Liu Wei;Xiong Changbing
1982, (4): 61-70.
PDF [ 566 K ]( 341 ) HTML
OPTIMAL GUIDANCE LAWS FOR MISSILES WITH SECOND ORDER CHARACTERISTICS
Li Zhongying
1982, (4): 71-83.
PDF [ 607 K ]( 270 ) HTML
AN OPTIMAL GUIDANCE LAW VIA FIRST ORDER INERTIAL LOOP
Chen Xueyu
1982, (4): 84-92.
PDF [ 511 K ]( 507 ) HTML
DEFORMATION WORK DENSITY FRACTURE CRITERION FOR COMPOSITE MATERIALS
Xue Kexing;Chou Jin
1982, (4): 93-100.
PDF [ 433 K ]( 1325 ) HTML
NUMERICAL CALCULATION OF LOCAL CONVECTIVE HEAT TRANSFER COEFFICIENTS OVER AIR-COOLED VANE SURFACES
Ling Junxiao;Jin Denian
1982, (4): 101-106.
PDF [ 340 K ]( 348 ) HTML
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