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25 December 1989, Volume 10 Issue 12

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25 December 1989, Volume 10 Issue 12

论文

AFFD TECHNOLOGY FOR NEW AIRPLANE DESIGN
Abstract( 1142 )

Wang Junyang;Zheng Minzhong

1989, (12): 565-569.

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NEW PROGRESS IN AIRFRAME DURABILITY REQUIREMENTS
Abstract( 1506 )

Wang Zheng

1989, (12): 570-575.

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A STUDY OF THE EFFECTIVEIY PROTECTIVE MEASURE TO PREVENT FRETTING DAMAGE OCCURRED IN HIGH STRENGTH ALUMINIUM-ALLOY RIVETED FASTENER
Abstract( 1114 )

Li Dongzi;Zhi Fuxiang;Liu Wenbing;Yang Liangui

1989, (12): 576-580.

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A STUDY ON THE BEHAVIOUR OF SMALL CRACK GROWTH AT THE EDGE OF A HOLE
Abstract( 1205 )

Li Zhengneng;Luo Fangyi

1989, (12): 581-586.

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ON THE PROBLEMS OF A PLATE WITH SURFACE CRACK AND REINFORCED BY AN ADHESIVE PATCH
Abstract( 1043 )

Chen Fuyao;Gao Yangshou

1989, (12): 587-594.

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A STUDY ON INITIAL FATIGUE QUALITY OF TYPICAL AIRCRAFT STRUCTURES （FASTENER HOLES）
Abstract( 1680 )

Tong Minbo;Zheng Minzhong;Wang Junyang;Chen Chuanyao

1989, (12): 595-600.

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J_n-INTERGRAL AND THE CONTROLLING PARAMETER FOR CRACK GROWTH
Abstract( 1117 )

Guan Zhongxin;Yang Xiaohua

1989, (12): 601-606.

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A STUDY OF SHEAR-BUCKLING FATIGUE FOR THIN-WALLED STRUCTURES
Abstract( 2076 )

Xue Jingchuan;He Gongtai;Song Xiangchen;Yang Yugong

1989, (12): 607-613.

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A CLOSED FORM SOLUTION OF STRESS INTENSITY FACTORS FOR THREE DIMENSIONAL FINITE BODIES WITH UNSYMMETRIC CRACKS BY ENERGY RELEASE RATE METHOD
Abstract( 1415 )

Wang Qizhi Zhang Xing;Ren Bingyi

1989, (12): 614-622.

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THE STATISTICAL DISTRIBUTION NATURE OF THE STATIC STRENGTH AND THE FATIGUE LIFE FOR THE LY12CZ ALLOY ALUM
Abstract( 1576 )

Xue Jingchuan;Jiao Kunfang;Qiu Jin

1989, (12): 623-630.

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NUMERICAL ANALYSIS FOR CRACK-STOPPING EFFECTS OF AN INTERFERENCE-FIT BUSHING ON AN ATTACHMENT LUG
Abstract( 1503 )

Hu Fangzong;Tang Longhua;Zhang Xiangzhou;Liu Xuehui

1989, (12): 631-635.

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AN EXPERIMENT STUDY FOR ENGINEERING SMALL CRACK GROWTH BEHAVIOR
Abstract( 1304 )

Zheng Minzhong;Nie Xuezhou;Liu Xiaoguang

1989, (12): 636-639.

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STUDIES ON THE OPTIMIZATION OF THE INTERFERENCE FIT OF A BOLT JOINT
Abstract( 1250 )

Liu Li;He Qingzhi;Jiu Luhe

1989, (12): 640-644.

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WEIGHT FUNCTION ANALYSIS FOR CRACKS AT A HOLE IN A FINITE PLATE
Abstract( 1149 )

Wu Xueren

1989, (12): 645-648.

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A STUDY ON FATIGUE DAMAGE AND CRACK INITIATION OF LY12CZ ALLOY
Abstract( 1333 )

Li Changchun;Zhao Huixia;Li Guangxia;Zheng Minzhong

1989, (12): 649-652.

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THE APPLICATION OF THE ENGINEERING APPROACH FOR ANALYZING CRACK TOLERANCE OF FUSELAGE PANELS TO A TRANSPORT AIRPLANE
Abstract( 1766 )

Lu Fumei;Wang Bin;Liu Diqing

1989, (12): 653-658.

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RESEARCH OF FATIGUE CRACK INITIATION GROWTH THRESHOLD
Abstract( 1612 )

Liu Wenting

1989, (12): 659-661.

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ELASTIC-PLASTIC ANALYSES OF FASTENER HOLES OF INTERFERENCE-FIT RIVETS AND ITS APPLICATION IN FATIGUE LIFE ESTIMATION
Abstract( 1080 )

Wu shen

1989, (12): 662-665.

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A METHOD OF THREE-PARAMETER POWER FUNCTION FOR FITTING a-N（a-t）CURVE
Abstract( 1347 )

Fu Huimin;Gao Zhentong

1989, (12): 666-670.

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THE INITIAION AND PROPAGATION OF SMALL CRACK AT THE EDGE OF A HOLE
Abstract( 1435 )

Lv Guozhi

1989, (12): 671-673.

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SOME DISCUSSIONS ABOUT THE FRACTURE CRITERIA OF MIXED-MODE CRACK BASED ON THE STRESS PARAMETER
Abstract( 1142 )

Su Bin;Cui Zhenyuan

1989, (12): 674-677.

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