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A SIMPLIFIED METHOD FOR PREDICTING ROTOR BLADE AIRLOADS
Wang Shicun;Xu Zhi
1982, (2): 1-17.
PDF [ 615 K ]( 407 ) HTML
STUDY ON PRESSURE DISTRIBUTION ON ROTOR BLADES WITH THREE-DIMENSIONAL NONSTEADY THEORY OF COMPRESSIBLE FLUID
Li Zhenhao;Ruan Tianen
1982, (2): 18-28.
PDF [ 653 K ]( 322 ) HTML
APPLICATION OF KALMAN FILTERING TECHNIQUE TO AERODYNAMIC DERIVATIVES FOR A HELICOPTER
Yang Songshan
1982, (2): 29-35.
PDF [ 429 K ]( 327 ) HTML
A FEASIBLE SIMPLIFIED METHOD FOR FINITE ELEMENT GRID OPTIMIZATION
Gong Yaonan
1982, (2): 36-42.
PDF [ 494 K ]( 269 ) HTML
THE CRACK-FREE LIFE PREDICTION FOR STRUCTURAL JOINTS UNDER CONSTANT AMPLITUDE LOADS
Xue Jingchuan;Yang Yugong
1982, (2): 43-50.
PDF [ 470 K ]( 826 ) HTML
AN ANALOGY METHOD FOR CRACK INITIATION LIFE PREDICTION
Zhang Fuze
1982, (2): 51-60.
PDF [ 323 K ]( 332 ) HTML
PDF [ 323 K ]( 227 ) HTML
A KIND OF TRANSITION FINITE ELEMENT FOR ANALYSIS OF SOLID-SHELL OR TENSILE PLATE-PLANE BEAM COMBINED STRUCTURES
Yin Zeyong;Yin Jing;Ren Peizheng
1982, (2): 72-82.
PDF [ 419 K ]( 275 ) HTML
PATTERNS OF MONOPULSE ARRAYS WITH TRIANGULAR AMPLITUDE DISTRIBUTION
L&#;Shanwei
1982, (2): 83-90.
PDF [ 502 K ]( 294 ) HTML
MODIFICATION OF THE WILLENBORG AND MAARSE MODELS AND APPLICATION TO THE LIFE PREDICTION FOR Ti-6Al-4V ALLOY
Zhang Yongkui;Gu Mingda;Yan Minggaoof
1982, (2): 91-99.
PDF [ 519 K ]( 268 ) HTML
STUDY ON THE MEASURING TECHNIQUE OF THIN BOUNDARY LAYERS
He Zhongwei
1982, (2): 100-104.
PDF [ 1141 K ]( 449 ) HTML
MICROMECHANICAL ANALYSIS OF CREEP CRACK GROWTH ON A NICKEL-BASE SUPERALLOY
Shen Huiwang;Gao Zhentao;Liu Changfu;Cai Qigung
1982, (2): 105-111.
PDF [ 2120 K ]( 333 ) HTML
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