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15 January 1994, Volume 1 Issue 1

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15 January 1994, Volume 1 Issue 1

论文

ON THE DEVELOPMENT OF AIRCRAFT STRENGTH SPECIFICATION
Abstract( 2938 )

Jiang Zuguo;Wang Ji;QuJianzhong;WangGenyuan;ZhangYonghe

1994, (1): 1-7.

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ON THE DEVELOPMENT OF AIRCRAFT STRENGTH SPECIFICATION
Abstract( 1111 )

Jiang Zuguo;Wang Ji;QuJianzhong;WangGenyuan;ZhangYonghe

1994, (1): 1-7.

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THE DLVELOPMENT AND DISCUSSION OF SOME QUESTIONS OF AIR CRAFT GROUND LOADS
Abstract( 1782 )

Gao Zejiong;Lin Hong;Zhao Shichun;Huang Zhenwei;Li Benxu

1994, (1): 8-16.

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INDENTIFICATION OF NONLINEAR PROPERTIES OF AN AIRCRAFT LANDING GEAR SHOCK STRUT
Abstract( 1574 )

Zhang Zengchang;Zhang Jiangjan

1994, (1): 17-22.

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INDENTIFICATION OF NONLINEAR PROPERTIES OF AN AIRCRAFT LANDING GEAR SHOCK STRUT
Abstract( 996 )

Zhang Zengchang;Zhang Jiangjan

1994, (1): 23-26.

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THE INFLUENCE OF AIRPLANE CONTROL SYSTEM PROPERTIES ON THE MANEUVER LOADS
Abstract( 1414 )

Wang Zhongyan

1994, (1): 27-31.

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ANALYTICAL INVESTIGATION OF THE AIRCRAFT FLIGHT LOADS
Abstract( 1312 )

Deng Lidong;Xu Chunsheng;Dong Xiurong

1994, (1): 32-35.

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STATISTICAL ANALYSIS OF MULTIPARAMETER FLIGHT DATA AND DETERMINATION OF FATIGUE LOAD STATES
Abstract( 1195 )

Liu Xiaodong;Shen Zhengjin

1994, (1): 36-40.

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A STUDY ON FLIGHT LOADS FOR UNSYMMETRICAL POWER MANEUVER
Abstract( 1274 )

Li Zhaoguang

1994, (1): 41-45.

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DEVELOPMENT AND APPLICATION OF AIRPLANK AIRLOAD CALCULATION SOFTWARE IN ACCORDANCE WITH NATIONAL MILITARY SPECIFICATION
Abstract( 1165 )

Cheng Gang

1994, (1): 46-49.

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SIMPLIFYING AND CONCENTRATING A SET OF RANDOM SPECTRUM FOR TRANSPORT
Abstract( 1073 )

Zhang Baofa;Fu Xiangjiong

1994, (1): 50-53.

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IDENTIFICATION OF AIRPLANE LANDING GEAR LOADS DURING TAXIING
Abstract( 1069 )

Zhang Zengchang;Zhang Jiangjan;Wang Yuchang

1994, (1): 54-61.

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A CALCULATION METHOD OF EQUIVALENT DAMAGE FOR LANDING GEAR FATIGUE LOAD SPECTRUM
Abstract( 1341 )

Su Kaixin

1994, (1): 62-69.

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THE PROFILE-ENVIRONMENT ANALYSIS METHOD FOR COMPILING AIRCRAFT OPERATIONAL ENVIROMENT SPECTRA
Abstract( 933 )

Jiang Zu guo

1994, (1): 70-75.

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THE COMPILATION OF AIRCRAFT LOAD-ENVIRONMENT SPECTRA
Abstract( 1049 )

Jiang Zuguo

1994, (1): 76-81.

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RELIABILITY AND RISK ANALYSIS OF REPAIRABLE AIRFRAME COMPONENTS
Abstract( 811 )

Lin Fujia;Zhou Xiaoyang

1994, (1): 82-88.

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APPROACH OF FUZZY RELIABILITY DESIGN FOR FATIGUE STRENGTH
Abstract( 1083 )

Han Enhou;Cui Guangchun

1994, (1): 89-93.

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FORMULAS FOR TOLERANCE LIMITS AND CONFIDENCE LIMITS OF NORMAL POPULATION PERCENTILES AND PERCENTAGES
Abstract( 1425 )

Fu Huimin

1994, (1): 94-101.

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THE OPTIMIZATION OF LOAD EQUATION DURING AIRCRAFT FLIGHT LOAD MEASUREMNT
Abstract( 1334 )

Hu Changrong

1994, (1): 102-105.

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ASTUDY ON FLIGHT LOAD ESTIMATION OF AIRCRAFT STRUCTURAL COMPONENTS
Abstract( 1397 )

Sun Jianhua;Qu Shihong

1994, (1): 106-108.

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A STUDY ON A PARAMETRIC IDENTIFICATION METHOD OF FLIGHT LOAD
Abstract( 1327 )

SunJianhua;QuShihong

1994, (1): 109-112.

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PROBLEMS STUDY──CONCERN OF STRENGTH SPECIFICATION APPLICATION
Abstract( 1062 )

Cao Kangjia

1994, (1): 113-115.

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A NEW FATIGUE CUMULATIVE DAMAGE DYNAMIC INTERFERENCE MODEL
Abstract( 1209 )

Liaomin;Yang Qingxiong

1994, (1): 116-120.

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THE CALCULATION METHOD RESEARCH OF AIRCRAFT WEAROUT LIFE
Abstract( 925 )

Zhang Xizhen

1994, (1): 121-123.

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LOAD DESIGN CHARACTERISTICS FOR FLY-BY-WIRE AIRCRAFT
Abstract( 766 )

Ma Baolin;Li Zhaoguang

1994, (1): 123-125.

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RESEARCH IN THE ANALYSIS METHOD OF ACOUSTIC FATIGUEFOR THE TYPICAL STRUCTURE OF MANEUVER AIRCRAFT UNDER THE ACTION OF AERODYNAMICAL NOISE
Abstract( 921 )

Zhang Xizhen

1994, (1): 125-127.

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ANALYTICAL INVESTIGATION IDEA OF UNLINEAR FLIGHT LOADS
Abstract( 786 )

Deng Lidong

1994, (1): 128-128.

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