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THE CALCULATION OF THREE-DLMENSIONAL COMPRESSIBLE BOUNDARY LAYER STABILITY ON SWEPT WINGS
Tang Deng-bin
1992, (1): 1-7.
PDF [ 426 K ]( 410 ) HTML
UNCONDITIONALLY STABLE TIME-STEP-TIME METHOD COMBINED WITH BOUNDARY ELEMENT TECHNIQUE FOR TRANSIENT HEAT CONDUCTION ANALYSIS
Huang Zheng-ming
1992, (1): 8-16.
PDF [ 503 K ]( 358 ) HTML
THE NUMERICAL SIMULATION OF COMPRESSIBLE FLOW AROUND AN AIRFOIL AT HIGH ANGLE OF ATTACK
Li Feng;Wang Yi-yun;Cui Er-jie
1992, (1): 17-22.
PDF [ 356 K ]( 860 ) HTML
COUPLED-MODE SUBSPACE PERTURBATION METHOD FOR STRUCTURE DYNAMIC MODIFICATION
Sun Jiu-hou;Zhu De-mao
1992, (1): 23-28.
PDF [ 346 K ]( 459 ) HTML
A METHOD OF FINITE ELEMENT MODEL UPDATING VIA DESIGN PARAMETERS
Zeng Qing-hua;Zhang Ling-mi
1992, (1): 29-35.
PDF [ 398 K ]( 498 ) HTML
MATERIAL NONLINEAR ANALYSIS OF LAMINATED PLATES AND SHELLS BY FINITE ELFMENT METHOD
Cao Da-wei;Jiang Xie-zhi
1992, (1): 36-41.
PDF [ 344 K ]( 402 ) HTML
A TIME MARCHING METHOD IN FINITE VOLUME FOR TRANSONIC DIFFUSER TURBULENT FLOWS
Zhang Shu-cheng;Huang Xi-jun
1992, (1): 42-47.
PDF [ 323 K ]( 368 ) HTML
A NEW METHOD FOR PREDICTING THE END WALL BOUNDARY LAYERS AND THE BLADE FORCE DEFECTS iNSIDE THE PASSAGE OF AXIAL COMPRESSOR CASCADES
Wu Hu;Chen Fu-qun;Liu Song-ling;Huang Zhi-tao
1992, (1): 48-56.
PDF [ 494 K ]( 360 ) HTML
BASIC ANALYSIS OF COUNTER-ROTATING TURBINES
Cai Jun-xian
1992, (1): 57-63.
PDF [ 399 K ]( 1212 ) HTML
A TMM FOR THE FREE VIBRATION OF SHELLS OF REVOLUTION
Cai Xian-xin
1992, (1): 64-70.
PDF [ 341 K ]( 434 ) HTML
A STUDY OF THE HOT EXTRUSION PROCESS OF ROD
Guo Nai-cheng;Luo Zi-jian
1992, (1): 71-79.
PDF [ 432 K ]( 385 ) HTML
A MODEL OF OPTIMIZING EQUILIBRIUM TRANSPORTATION NETWORK IN DESIGN
Huang Hai-jun;Chen Liang-you
1992, (1): 80-86.
PDF [ 413 K ]( 584 ) HTML
AN IMPROVED MULTIPLE LINE-VORTEX METHOD FOR SIMULATION OF SEPARATED VORTICES OF SLENDER WINGS
Guo Wen-hai;Xing Ding-ding;Zhuang Feng-gan
1992, (1): 87-90.
PDF [ 232 K ]( 467 ) HTML
AERODYNAMIC SENSITIVITIES FOR SUBSONIC LIFTING-SURFACE
Xu Ming-chu;Gu Wen-ying
1992, (1): 91-95.
PDF [ 303 K ]( 427 ) HTML
RATIONAL INTERPOLATION METHOD FOR INTERACTIVE SHAPE DESIGN
Kang Bao-sheng
1992, (1): 96-100.
PDF [ 265 K ]( 323 ) HTML
STUDY ON TWO VARIABLE CONTROL PLAN FOR TWIN SPOOL TURBOJET ENGINE
Zhang Jia-zhen;Hua Kai;Huang Xian
1992, (1): 101-105.
PDF [ 313 K ]( 489 ) HTML
VARIABLE STRUCTURE CONTROL FOR A CLASS OF NONLINEAR CONTROL SYSTEMS
Yao Yu;Wang Zi-cai
1992, (1): 106-111.
PDF [ 306 K ]( 368 ) HTML
THE FAILURE THRESHOLD SELECTION IN FAULT DETECTION OF REDUNDANT CONTROL SYSTEMS
Niu Pei-yi
1992, (1): 112-116.
PDF [ 287 K ]( 584 ) HTML
EFFECT OF WIDE CHANGE OF COOLING RATE ON DENDRITIC SEGREGATION OF A DIRECTIONALLY SOLIDIFIED COBALT-BASE SUPERALLOY
Li Jian-guo;Chu Shuang-jie;Liu Zhong-yuan;Fu Heng-zhi
1992, (1): 117-120.
PDF [ 310 K ]( 843 ) HTML
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