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25 December 1991, Volume 12 Issue 12

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25 December 1991, Volume 12 Issue 12

论文

AN EXPERIMENTAL STUDY ON FATIGUE LIFE OF INTERFERENCE-FIT COMPOSITE JOINT
Abstract( 1722 )

Liu Ping;Zhang Kaida

1991, (12): 545-549.

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EXPERIMETAL INVESTIGATION ON FLUTTER CHARACTERISTICS OF COMPOSITE TORSION-BOX
Abstract( 1721 )

Zhu Fenghui;Qiu Tao

1991, (12): 550-553.

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STRUCTURAL OPTIMIZATION AND VIBRATION CONTROL OF COMPOSITE ROTOR BLADES
Abstract( 2304 )

Fan Guaaghua;Hou Ruliang;Cheng Gengdong

1991, (12): 554-559.

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EXPERIMENTAL STUDY ON THE EFFECT OF STACKING SEQUENCE ON THE CARRYING CAPACITY OF THE LAMINATED STRUCTURE
Abstract( 2366 )

Xie Mingjiu;Zhu Liping;Shi Lizhong

1991, (12): 560-564.

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CARBON-FIBER-REINFORCED ALUMINIUM MATRIX COMPOSITES BY CASTING
Abstract( 2631 )

Li Hualun;Shang Baolu;Mao Zhiying;Zhou Yaohe

1991, (12): 565-569.

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CONTROL OF INTERFACE REACTIONS BETWEEN P-55 FIBERS AND ALUMINIUM ALLOY MATRICES DURING PRESSURE INFILTRATION PROCESSING
Abstract( 1376 )

Zhang Guoding;Feng Shaoren;J. A. Cornie

1991, (12): 570-575.

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MOISTURE ABSORPTION CHARACTERISTICS OF HYBRID COMPOSITES
Abstract( 1495 )

Zhang Zuoguang;Song Huancheng;Li Hongyun

1991, (12): 576-582.

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EVALUATION OF THE TOUGHNESS OF QY8911 BISMALEIMDE
Abstract( 1832 )

Beijing Aeronautical Manufacture Technology Zhao Qusen

1991, (12): 583-588.

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DEVELOPMENT AND APPLICATION OF A FIBER REINFORCED ALUMINIUM LAMINATES
Abstract( 2132 )

Chen Shaojie;Zhu Shan;Li Ping

1991, (12): 589-597.

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STABILITY OF THIN CIRCULAR CYLINDRICAL SHELLS COMPOSED OF COMPOSITE MATERIALS
Abstract( 1594 )

Wang Junkui;Wang Hu

1991, (12): 598-605.

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THE INVESTIGATION OF DAMAGE IN LAMINATES DUE TO LOW VELOCITY IMPACT
Abstract( 1874 )

Zheng Chuanchao;Zhang Kaida;Liu Xuehui

1991, (12): 606-609.

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THERMAL BUCKLING OF ANTISYMMETRIC CROSS-PLY LAMINATED COMPOSITE PLATES
Abstract( 1356 )

Sun Liangxin;Ma Lingjian

1991, (12): 610-615.

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ANALYSIS OF STEADY MOISTURE AND STRESS FIELD FOR COMPOSITE LAMINATED PLATES
Abstract( 1318 )

Wang Quanrong;Cheng Wanzhi;Sun Yanbo;Chen Haoran;Xi Zhichen

1991, (12): 616-619.

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DAMAGE TOLERANCE AND DURABILITY DESIGN OF COMPOSITE AIRCRAFT STRUCTURES
Abstract( 1762 )

Shen Zhen;Tang Xiaodong;Chen Puhui

1991, (12): 620-622.

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ANALYSIS OF TENSILE STRENGTH OF LAMINATES WITH A HOLE TAKING INTO ACCOUNT THE EDGE-EFFECT
Abstract( 1451 )

Li Shunlin;Xiong Zhongkan

1991, (12): 623-627.

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A REVIEW OF SOME COMPUTER PROGRAMS OF COMPOSITES
Abstract( 1079 )

Zhang Linrui

1991, (12): 628-630.

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SAFETY FACTOR AND RELIABILITY FOR COMPOSITE LAMINATES
Abstract( 1498 )

Yang Ling;Ma Zukang;Fu Guozheng

1991, (12): 631-634.

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STUDY OF DYNAMIC STRENGTH ON COMPOSITE WING
Abstract( 1502 )

He Lianzhu

1991, (12): 635-638.

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ENGINEERING METHOD RESEARCH OF POST-BUCKLING STRENGTH FOR COMPOSITE STIFFENED PANELS
Abstract( 1355 )

Zhu Jufen;Chen Haoran Chen Shao jie;Cheng Wanzhi

1991, (12): 639-642.

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EXPERIMENTAL STUDY ON FATIGUE BEHAVIOUR OF COMPOSITE LAMINATE
Abstract( 1364 )

Chai Yanan;Shen Zhenand Li Shunhe

1991, (12): 643-646.

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DESIGN VARIABLES AND CONSTRAINT DERIVATIVES IN AEROELASTIC TAILORING
Abstract( 1487 )

Gao Ping;Zhang Zhilong

1991, (12): 647-650.

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INVESTIGATION ON MECHANISM FOR ELECTRICAL DISCHARGE MACHINING OF CARBON FIBRE COMPOSITE MATERIAL
Abstract( 2331 )

Wang Min;Lau W.S.

1991, (12): 651-654.

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INVESTIGATION ON MICROWAVE ABSORBER WITH ADDITIVE OF METAL COATED CARBON FIBER
Abstract( 1956 )

Yi Pei;Gan Yongxue

1991, (12): 655-657.

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