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25 March 1993, Volume 14 Issue 3

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25 March 1993, Volume 14 Issue 3

论文

DYNAMIC FRACTURE ANALYSIS OF A MULTIPLE-STIFFENED PANEL WITH A CENTRAL CRACK
Abstract( 2095 )

Wang Yuan-han;Liu Zai-hua;Wang Jian

1993, (3): 113-119.

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THE STOCHASTIC CRACK GROWTH ANALYSIS OF A TYPICAL STRUCTURAL DETAIL-FASTENER HOLE OF AIRCRAFT STRUCTURE
Abstract( 2304 )

Li Zhong;Wu Xiao-feng;Zheng Min-zhong

1993, (3): 120-126.

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THE STRESS INTENSITY FACTORS FOR EDGE CRACKS IN STIFFENED PLATES
Abstract( 2603 )

Huang Wei-yang;Yan Guo-lin

1993, (3): 127-133.

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THE RESEARCH ON A MODEL OF PROBABILITY DAMAGE TOLERANCE ANALYSIS
Abstract( 2355 )

Liu Wen-ting;Luo yi;Tong Ming-bo

1993, (3): 134-139.

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A STATISTICAL MODEL OF FATIGUE CRACK GROWTH UNDER RANDOM LOADING
Abstract( 2263 )

Liao Min;Yang Qing-xiong

1993, (3): 140-146.

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ANALYTICAL-GENERALIZED VARIATIONAL METHOD ABOUT SOLUTION OF SIF AND CONSERVATIVE INTEGRAL FOR DELAMINATIONS OF LAMINATE BEAM
Abstract( 1976 )

Meng Qing-chun;Zhang Xing

1993, (3): 147-154.

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A MODEL FOR THE RELIABILITY ANALYSIS OF STRUCTURES UNDER RANDOM STRESS RANGE LOADINGS (RDCDR MODEL)
Abstract( 2115 )

Xu Guo-jian;Gao Zhen-tong

1993, (3): 155-160.

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A CYCLE COUNTING METHOD FOR CYCLE BY CYCLE CRACK GROWTH ANALYSIS
Abstract( 2002 )

Zhu Yi-gang;Zhang Shi-jie;Yan Ming-gao

1993, (3): 161-165.

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A METHOD OF TWO-DIMENSIONAL ONE-SIDED TOLERANCE FACTORS
Abstract( 2618 )

Fu Hui-min

1993, (3): 166-172.

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A FORMULA OF THREE-PARAMETER POWER FUNCTION FOR ε-N CURVES
Abstract( 3467 )

Fu Hui-min

1993, (3): 173-176.

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STRESS INTENSITY FACTOR ANALYSIS FOR STIFFENED PANEL WITH A CIRCULAR HOLE
Abstract( 2253 )

Xu Jia-yao;Wang Ke

1993, (3): 177-184.

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A STUDY ON THE RELATION BETWEEN TWO KINDS OF RELIABILITY INDEXES
Abstract( 2490 )

Xue Jing-chuan;Jiao Kun-fang;Feng Yun-weng

1993, (3): 185-187.

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CRACK PROPAGATION AND LIFE PREDICTION UNDER CORROSION FATIGUE
Abstract( 2612 )

Wang Rong;Lou Ming-xiu;Zheng Xiu-lin

1993, (3): 188-192.

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THE INFLUENCE OF LASER RADIATION ON THE FATIGUE-FRACTURE PROPERTY OF LY12CZ Al-ALLOY
Abstract( 2552 )

Guo Zhi-de;He Qiu-juLi Guang-xia;Li Chang-chun

1993, (3): 193-196.

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STATISTICAL ANALYSIS OF FATIGUE CRACK GROWTH DATA
Abstract( 2455 )

Wang Zhi-zhi;Nie Xue-zhou;Wu Xiao-feng

1993, (3): 197-201.

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THE GENERAL SITUATION OF DESIGN AND TEST TECHNIQUE DEVELOPMENT ON CIVIL AIRCRAFT DURABILITY AND DAMAGE TOLERANCE OF PREVIOUS USSR
Abstract( 3758 )

Xue Jing-chuan;Xue Tie-jun;Zheng Wen-zhong

1993, (3): 202-204.

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FATIGUE LIFE INCREMENT OF INTERFERENCE FIT TAPERED SHANK BOLT CONNECTIONS UNDER RANDOM LOADING
Abstract( 2622 )

Xiao Shou-ting;Fu Xiang-jiang;Liu Yi-bing

1993, (3): 205-210.

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THE RELIABILITY MODEL OF THE STRUCTURE WITH MULTI-CRACKS UNDER RANDOM LOADS
Abstract( 2199 )

Fei Bin-jun;Gao Zhen-tong

1993, (3): 211-214.

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A STUDY ON STATISTICAL NATURE OF FATIGUE CRACK GORWTH FOR THE LY12CZ AND LC4CS ALLOYS ALUMINUM
Abstract( 2398 )

Liu Xiu-li;Lu Fu-mei;Wu Xiao-feng

1993, (3): 215-218.

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THE STATISTICAL ANALYSIS OF RANDOM CRACK GROWTH FOR WING PANELS
Abstract( 2216 )

Liu Xiu-li;Lu Fu-mei;Wu Xiao-feng;Wang Bin

1993, (3): 219-222.

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