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ON THE DEVELOPMENT OF AIRCRAFT STRENGTH SPECIFICATION
Jiang Zuguo;Wang Ji;QuJianzhong;WangGenyuan;ZhangYonghe
1994, (1): 1-7.
PDF [ 500 K ]( 885 ) HTML
THE DLVELOPMENT AND DISCUSSION OF SOME QUESTIONS OF AIR CRAFT GROUND LOADS
Gao Zejiong;Lin Hong;Zhao Shichun;Huang Zhenwei;Li Benxu
1994, (1): 8-16.
PDF [ 497 K ]( 526 ) HTML
INDENTIFICATION OF NONLINEAR PROPERTIES OF AN AIRCRAFT LANDING GEAR SHOCK STRUT
Zhang Zengchang;Zhang Jiangjan
1994, (1): 17-22.
PDF [ 304 K ]( 314 ) HTML
1994, (1): 23-26.
PDF [ 306 K ]( 400 ) HTML
THE INFLUENCE OF AIRPLANE CONTROL SYSTEM PROPERTIES ON THE MANEUVER LOADS
Wang Zhongyan
1994, (1): 27-31.
PDF [ 400 K ]( 439 ) HTML
ANALYTICAL INVESTIGATION OF THE AIRCRAFT FLIGHT LOADS
Deng Lidong;Xu Chunsheng;Dong Xiurong
1994, (1): 32-35.
PDF [ 273 K ]( 1471 ) HTML
STATISTICAL ANALYSIS OF MULTIPARAMETER FLIGHT DATA AND DETERMINATION OF FATIGUE LOAD STATES
Liu Xiaodong;Shen Zhengjin
1994, (1): 36-40.
PDF [ 336 K ]( 366 ) HTML
A STUDY ON FLIGHT LOADS FOR UNSYMMETRICAL POWER MANEUVER
Li Zhaoguang
1994, (1): 41-45.
PDF [ 424 K ]( 586 ) HTML
DEVELOPMENT AND APPLICATION OF AIRPLANK AIRLOAD CALCULATION SOFTWARE IN ACCORDANCE WITH NATIONAL MILITARY SPECIFICATION
Cheng Gang
1994, (1): 46-49.
PDF [ 312 K ]( 637 ) HTML
SIMPLIFYING AND CONCENTRATING A SET OF RANDOM SPECTRUM FOR TRANSPORT
Zhang Baofa;Fu Xiangjiong
1994, (1): 50-53.
PDF [ 324 K ]( 424 ) HTML
IDENTIFICATION OF AIRPLANE LANDING GEAR LOADS DURING TAXIING
Zhang Zengchang;Zhang Jiangjan;Wang Yuchang
1994, (1): 54-61.
PDF [ 398 K ]( 468 ) HTML
A CALCULATION METHOD OF EQUIVALENT DAMAGE FOR LANDING GEAR FATIGUE LOAD SPECTRUM
Su Kaixin
1994, (1): 62-69.
PDF [ 446 K ]( 529 ) HTML
THE PROFILE-ENVIRONMENT ANALYSIS METHOD FOR COMPILING AIRCRAFT OPERATIONAL ENVIROMENT SPECTRA
Jiang Zu guo
1994, (1): 70-75.
PDF [ 393 K ]( 384 ) HTML
THE COMPILATION OF AIRCRAFT LOAD-ENVIRONMENT SPECTRA
Jiang Zuguo
1994, (1): 76-81.
PDF [ 415 K ]( 741 ) HTML
RELIABILITY AND RISK ANALYSIS OF REPAIRABLE AIRFRAME COMPONENTS
Lin Fujia;Zhou Xiaoyang
1994, (1): 82-88.
PDF [ 402 K ]( 399 ) HTML
APPROACH OF FUZZY RELIABILITY DESIGN FOR FATIGUE STRENGTH
Han Enhou;Cui Guangchun
1994, (1): 89-93.
PDF [ 378 K ]( 425 ) HTML
FORMULAS FOR TOLERANCE LIMITS AND CONFIDENCE LIMITS OF NORMAL POPULATION PERCENTILES AND PERCENTAGES
Fu Huimin
1994, (1): 94-101.
PDF [ 410 K ]( 619 ) HTML
THE OPTIMIZATION OF LOAD EQUATION DURING AIRCRAFT FLIGHT LOAD MEASUREMNT
Hu Changrong
1994, (1): 102-105.
PDF [ 332 K ]( 607 ) HTML
ASTUDY ON FLIGHT LOAD ESTIMATION OF AIRCRAFT STRUCTURAL COMPONENTS
Sun Jianhua;Qu Shihong
1994, (1): 106-108.
PDF [ 188 K ]( 485 ) HTML
A STUDY ON A PARAMETRIC IDENTIFICATION METHOD OF FLIGHT LOAD
SunJianhua;QuShihong
1994, (1): 109-112.
PDF [ 339 K ]( 617 ) HTML
PROBLEMS STUDY──CONCERN OF STRENGTH SPECIFICATION APPLICATION
Cao Kangjia
1994, (1): 113-115.
PDF [ 234 K ]( 484 ) HTML
A NEW FATIGUE CUMULATIVE DAMAGE DYNAMIC INTERFERENCE MODEL
Liaomin;Yang Qingxiong
1994, (1): 116-120.
PDF [ 403 K ]( 505 ) HTML
THE CALCULATION METHOD RESEARCH OF AIRCRAFT WEAROUT LIFE
Zhang Xizhen
1994, (1): 121-123.
PDF [ 262 K ]( 411 ) HTML
LOAD DESIGN CHARACTERISTICS FOR FLY-BY-WIRE AIRCRAFT
Ma Baolin;Li Zhaoguang
1994, (1): 123-125.
PDF [ 274 K ]( 389 ) HTML
RESEARCH IN THE ANALYSIS METHOD OF ACOUSTIC FATIGUEFOR THE TYPICAL STRUCTURE OF MANEUVER AIRCRAFT UNDER THE ACTION OF AERODYNAMICAL NOISE
1994, (1): 125-127.
PDF [ 191 K ]( 342 ) HTML
ANALYTICAL INVESTIGATION IDEA OF UNLINEAR FLIGHT LOADS
Deng Lidong
1994, (1): 128-128.
PDF [ 99 K ]( 482 ) HTML
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