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A TECHNIQUE OF DYNAMIC MODIFICATION FOR MISSILE-TRAILER SYSTEMS
Yao Changren Ma Yongping
1989(2): 1-8.
Abstract
PREDICTING VIBRATIONS OCCURING ON A MISSILE TRANSPORTER
Sun Changyan
1989(2): 9-16.
Abstract
A STUDY ON THE MAGNETIC FORCE OF PNEUMATIC SOLENOID VALVE
Sheng Yongcai Zhang Shoucai
1989(2): 17-23.
Abstract
STABILITY OF CIRCULAR CYLINDRICAL SHELLS WITH ELLIPTIC CUTOUTS
Li Mingxing Huang Yiming
1989(2): 24-28.
Abstract
WIND TUNNEL EXPERIMENTAL INVESTIGATION OF LOW DRAG EXTENDED RANGE PROJECTILES
Wu Jiasheng Xu Wenxi Ju Xianming
1989(2): 29-34.
Abstract
MOTION STABILITY CRITERION OF MISSILE BODY MITH VARIABLE PARAMETERS
Kang J ingli
1989(2): 35-40.
Abstract
AN APPROXIMATE METHOD OF DECOUPLING LONGITUDINAL AND LATERAL MOTIONS OF ROLLING MISSILES
Yuan Zihuai
1989(2): 41-50.
Abstract
EXPERIMENTAL STUDIES IN OPERATIONAL PERFORMANCE OF A STRAND BURNER SYSTEM
Zhang Ping Zhang Xunwen Zhang Qunxing Zhou Shengguo
1989(2): 51-56.
Abstract
ANALYSIS AND DESIGN OF A HIGH PRESSURE REDUCER VALVE FOR PNEUMATIC ACTUATOR
Cheng Hanchao
1989(2): 57-62.
Abstract
WIND TUNNEL EXPERIMENTAL TECHNIQUE FOR THE PITCHING DYNAMIC DERIVATIVES OF A SPINNING PROJECTILE HAVING HIGH FINENESS RATIO
Xu Wenxi Wu Jiasheng Ju Xianming
1989(2): 63-67.
Abstract
HEAT PROTECTION DESIGN AND EXPERIMENTAL RESEARCH OF A HIGH-PRESSURE GAS GENERATOR
Wang Chunli Zhou Shengguo
1989(2): 68-71.
Abstract
THE EFFECT OF ACCELERATION ON THE COMBUSTION OF ALUMINIZED COMPOSITE SOLID PROPELLANTS
Zhang Ruzhou Li Baojiang Zheng Xiaoping Li Kuiwu
1989(2): 72-76.
Abstract
MODAL DENSITY OF HONEYCOMB CYLINDERS
Yao Deyuan Pang Haishao Liu Suwen
1989(2): 77-81.
Abstract
DESIGN OF THE GUN ACCELERATOR
Gao Mingkun
1989(2): 82-86.
Abstract
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