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DAMAGE MECHANICS FINITE ELEMENT METHOD FOR PREDICTION OF TOTAL FATIGUE LIVES OF METAL STRUCTURE MEMBERS
Zheng Xudong;Zhang Xing
1991, (2): 1-9.
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AN EXPERIMENTAL RESEARCH ON BOLT HOLE STRENGTHENING OF TC-4 TITANIUM ALLOY
She Gongfan;Tao Hua;Zhang Jianjiang;Lin Shuifu
1991, (2): 10-15.
AN EXPERIMENTAL STUDY ON FATIGUE CRACK GROWTH FOR ENGINEERING SMALL CRACKS UNDER ELASTO-PLASTIC CONDITION
Zheng Minzhong;Nie Xuezhou;Liu Xiaoguang
1991, (2): 16-21.
THE EXACT SOLUTIONS FOR A CRACKED PLATE UNDER CONCENTRATED FORCES
Huang Weiyang
1991, (2): 22-26.
AN IMPACT DYNAMICS INVESTIGATION ON SOME PROBLEMS IN BIRD STRIKE ON WINDSHIELDS OF HIGH SPEED AIRCRAFTS
Wang Lili;Zhu Xixiong;Shi Shaoqiu;Gan Su;Bao Hesheng
1991, (2): 27-33.
THE INFLUENCE OF LASER RADIATION ON THE FATIGUE LIFE OF STEEL SPECIMENS
Li Xiping;Li Guangxia;Li Changchun;Guo Zhide
1991, (2): 34-38.
AN EXPERIMENTAL STUDY OF LASER STRENGTHENING TECHNOLOGY
Guo Zhide;He Qiuju;Li Guangxia;Li Changchun
1991, (2): 39-43.
SOLUTION OF STRESS INTENSITY FACTOR BY WEIGHT FUNCTION FOR SMALL SURFACE CRACKS IN PLATES
Zhao Wei;Wu Xueren;Yan Minggao
1991, (2): 44-49.
THE METHOD OF X~2 MINIMUM VALUE FOR ESTIMATING POPULATION PARAMETERS
Ling Jing;Gao Zhentong
1991, (2): 50-55.
MEASUREMENTS AND CALCULATIONS OF RESIDUAL STRESSES AT THE EDGES OF COLD-WORKED HOLES
Xing Wenzhen;Wu Fumin
1991, (2): 56-60.
AN ANALYSIS OF BONDED REPAIRS FOR CRACKED SHEETS WITH COMPOSITE PATCH
Jiang Jinlong;Zhao Mingpan
1991, (2): 61-67.
A STUDY ON THE EFFECTIVELY PROTECTIVE MEASURE TO PREVENT FRETTING DAMAGE IN LY12CZ LAP JOINTS WITH INTERFERENCE-FIT BOLT
Li Dongzi;Wang Jiansheng;Zi Fuxiang;Chen Gouding;Liu Wenbin
1991, (2): 68-72.
BIRD IMPACT ANALYSIS OF AIRCRAFT WINDSHIELD TRANSPARENCY
Gong Yaonan;Xu Suqiang
1991, (2): 73-78.
FATIGUE LIFE ESTIMATION UNDER COMPLEX LOADING
Tian Dingshuan;Wu Fumin
1991, (2): 79-86.
AN ELASTIC PLASTIC FINITE ELEMENT ANALYSIS OF CRACKED STIFFENED CURVED PANEL UNDER BIAXIAL STRESS
Wang Demin;Guan Zhongxin
1991, (2): 87-93.
THE MEASUREMENTS OF THE PROPAGATION AND CLOSURE OF FATIGUE SMALL CRACKS AT NOTCHES
He Youqing;Li Zhengneng;Kou Changhe;He Qingzhi
1991, (2): 94-99.
A STUDY OF DYNAMIC RESPONSE FOR BIRD IMPACT ON ARC WINDSHIELDS OF AIRCRAFTS
Zhang Qiqiao;Xu Zongqing
1991, (2): 100-105.
AN ANALYSIS OF THE CRACK PROPAGATION LIFE OF THE INTERFERENCE-FITTED FASTENER
Guo Wuanlin;Fu Xiangjiong
1991, (2): 106-111.
APPLICATION OF EXTRUSION STRENGTHENING TECHNIQUE ON INCREASING LIFE OF WING-OIL-DIVISION
Beijing University of Aeronautics and AstronauticsLiu WentingChengdn Aircraft Company Li Jinhua
1991, (2): 112-114.
A STUDY ON SHORT FATIGUE CRACK GROWTH AT THE EDGE OF A NOTCH
Li Changchun;Zhao Huixia;Li Guangxia;Zheng Minzhong
1991, (2): 115-119.
EQUIVALENT NOMINAL STRESS AND DETERMINATION OF STRUCTURAL DFR UNDER VARIABLE AMPLITUDE
Chu Kanghong;Xue Jingchuan
1991, (2): 120-122.
A METHOD OF INFINITE-LIFE RELIABILITY ANALYSIS
Fu Huimin;Gao Zhengtong;He Zhimin
1991, (2): 123-126.
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