AN ENGINEERING APPROACH FOR NEARLY SHOCK-FREE WING DESIGN
Zhu Ziqiang Beijing University of Aeronautics and Astronautics H. Sobieczky DFVLR Gottingen;F. R. Germany

..............page:81-86

THE STUDY OF THE GLOBAL STABILITY OF HIGH PERFORMANCE AIRCRAFT AT HIGH ANGLES-OF-ATTACK
Gao Hao and Zhou Zhiqiang Northwestern Polytechnical University

..............page:87-101

AN OPTIMUM METHOD FOR EXTRACTING THE AERODYNAMIC DERIVATIVES OF A HELICOPTER FROM FLIGHT TEST DATA
Yang Songshan Flight Test Research Institute

..............page:102-109

EXPERIMENTAL STUDY ON APPLICABILITY OF DAMAGE FAILURE CRITERION OF COMPOSITE LAMINATES
Shen Zhen;Liu Junshi and Tang Xiaodong. Aircraft Strength Research Institute Huang Qi and Shen Wei Huazong University of Science and Technology

..............page:110-113

STUDIES ON CYCLIC FATIGUE CHARACTERISTICS OF MATERIALS
Chen Zhiwei Aeronautical Engineering Research Institute;PLAAF;China

..............page:114-120

PULSE MEASURING TECHNIQUE FOR THE VIBRATION OF ROTOR BLADES IN MOTION
Zhang Yisong and Yi Liyan Nanjing Aeronautical Institute

..............page:121-126

NUMERICAL CALCULATION OF A CLASS OF OPTIMAL FLIGHT TRAJECTORIES
Wang Peide;Cui Taorui and Hou Ming Northwestern Polytechnical University

..............page:127-134

FATIGUE CRACK GROWTH BEHAVIOUR OF 7475-T7351 AL ALLOY UNDER CONSTANT AMPLITUDE LOADING
Zhang Shijie Institute of Aeronautical Materials;Beijing Marissen R. Schulte K. Trautmann K.H. Nowack H. Institute of Materials Research;DFVLR;FRG

..............page:135-144