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THEORETICAL ANALYSIS FOR RETARDING CRACK GROWTH BY ADHESIVELY BONDING STRIPS
Liu Tierang;Fan Weixun
1994, (3): 257-263.
PDF [ 372 K ]( 527 ) HTML
FATIGUE LIFE ESTIMATE UNDER RANDOM LOADING BASED ON PLASTIC HYSTERESIS ENERGY PRINCIPLE
Wu Fumin;Tian Dingshuan
1994, (3): 264-268.
PDF [ 173 K ]( 757 ) HTML
BOUNDARY ELEMENT METHOD SIMULATION AND CORROSION FATIGUELIFE PREDICTION FOR 3-D BLUNT CRACKS
Zhang Yongyuan;Ruan Guohua
1994, (3): 269-274.
PDF [ 320 K ]( 410 ) HTML
A DESTRUCTIVE EXPERIMENTAL STUDY OF THE ATTENUATION OF RESIDUAL STRESS AT AND NEAR THE EDGE OF A COLD EXPANDED HOLE UNDER APPLIED CYCLELOADING
Xing Wenzhen;Liu Yibing
1994, (3): 275-279.
PDF [ 373 K ]( 438 ) HTML
MART COMPOSITE STRUCTUREW OF SELF-ADAPTIVE STRENGTH
Tao Baoqi;Liang Dakai;Tao Yungang;Qing Taiyan;Wang Zheng;Yuan Shenfang
1994, (3): 280-286.
PDF [ 409 K ]( 604 ) HTML
AN ANALYTICAL-VARIATIONAL METHOD FOR ANISOTROPIC PLATES WITH UNSYMMETRIC DOUBLE EDGE CRACKS SUBJECTED TO PIN LOADS
Cui Deyu;ZhangXing
1994, (3): 287-294.
PDF [ 410 K ]( 494 ) HTML
LINEAR VARIANCE REGRESSION ANALYSIS
Fu Huimin
1994, (3): 295-302.
PDF [ 355 K ]( 921 ) HTML
CALCULATION OF CRACK DENSITY AND MANIPULATION OF ANGLE-PLIEDLAMINA FOR COMPOSITE LAMINATES WITH CONSTRAINED CRACKING
Hua Yu;He Qingzhi;Li Zhengneng;Kou Changhe
1994, (3): 303-309.
PDF [ 375 K ]( 521 ) HTML
AN ANALYTICAL METHOD OF PIN LOAD COMPUTATIONS FOR JOINTS WITH MULTI-FASTENERS
Jiang Chiping;Zhang Xing
1994, (3): 310-317.
PDF [ 404 K ]( 668 ) HTML
THE RELIABILITY AND DAMAGE TOLERANCE ANALYSIS OF AIRCRAFT PROPELLER
Fei Binjun;Gao Zhengtong
1994, (3): 318-323.
PDF [ 361 K ]( 433 ) HTML
STUDY ON EVALUATION METHOD OF WEAR RELIABILITY FOR LOCK MECHANISM SYSTEM OF CARGO-BRIDGE
Ouyang Zuxing;Yi Mingde
1994, (3): 324-330.
PDF [ 335 K ]( 475 ) HTML
PREDICTION OF THE TRUE SURVIVAL PROBABILITY CORRESPONDING TO THE ONE-SIDED TOLERANCE LIMIT
Lin Fujia;Li Zhuzhao
1994, (3): 331-335.
PDF [ 290 K ]( 850 ) HTML
THE PERFORMANCE TEST RESEARCH OF THE FATIGUE LIFE GAUGE
HuMingmin;Chen Jie;Tao Baoqi
1994, (3): 336-339.
PDF [ 365 K ]( 773 ) HTML
FATIGUE CRACK CLOSURE MEASUREMENTS ON 2024T3SHEET SPECIMENS
Wu Yisheng;J. Schijve
1994, (3): 340-343.
PDF [ 315 K ]( 675 ) HTML
A RELIABILITY ANALYSIS METHOD ON THE FATIGUE LIVES OF INTERFERENCE-FIT OR COLDWORKING STRENGTHENED PARTS
Guan Zhidong;He Qingzhi;LiZhengneng
1994, (3): 344-347.
PDF [ 256 K ]( 416 ) HTML
A STUDY ON IMPROVEMENT OF FATIGUE STRENGTH OF AERONAUTICAL STRUCTURE STEELS BY LASER TREATMENT
Tang Yaxin;Liu zhidong;Zhang Bin;Wu Yongduan;Yu Chenye
1994, (3): 348-352.
PDF [ 386 K ]( 366 ) HTML
STRESS INTENSITY FACTORS FOR AN INFINITE PLATE WITH TWO RANDOMLY POSITIONED CRACKS
Yan Guolin;Nuang Weiyang
1994, (3): 353-358.
PDF [ 302 K ]( 521 ) HTML
NEURAL NETWORK METHOD FOR FITTING FATIGUE EXPERIMENTAL CURVES
Wang Xiantong;Yang Qingxiong
1994, (3): 359-361.
PDF [ 308 K ]( 613 ) HTML
A STUDY ON EIFS DISTRIBUTION OF AIRCRAFT STRUCTURE DETAILS
Li Yumin;Shen Lizhong;Shi Rongming
1994, (3): 362-365.
PDF [ 320 K ]( 448 ) HTML
RESEARCH ON THE RELATIONSHIPS BETWEEN DFR AND OTHER FATIGUE PARAMETERS UNDER CONSTANT STRESS RATIOS
Dong Dengke;Xue Jingchuan;Yang Yugon
1994, (3): 366-371.
PDF [ 288 K ]( 559 ) HTML
ANALYSIS OF FATIGUE CRACK-GROWTH BEHAVIOUR IN CORNER CRACKS AT HOLES
Li Zhengneng;He Youqing
1994, (3): 372-375.
PDF [ 353 K ]( 373 ) HTML
EFFECT OF ENVIRONMENT MEDIUM AND STRESS RATIO ON CF CRACK INITIATION LIFE FOR 300M STEEL
Lu Minxu;Zheng Xiulin
1994, (3): 378-382.
PDF [ 427 K ]( 479 ) HTML
PRELIMINARY TO LIFE EVALUATION OFAIRFRAME FOR ULTRALIGHT AIRCRAFT
Wei Zhiyi
1994, (3): 382-384.
PDF [ 107 K ]( 450 ) HTML
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