1672-9897
1999 Issue 2
..............page:89-95
An Engineering Calculation Method of the Effect of Reynolds Number on Longitudinal Aerodynamic Characteristics of Aircraft with High Sweep and Low Aspect Ratio
Chen Dehua;Zhao Xiehe
Chen Dehua;Zhao Xiehe
..............page:83-89
..............page:79-82
The Use of the Thin Layer Model for Numerical Simulation of the Flow Around Three-Dimensional Bodies
T.A.科罗达耶娃;A.P.夏什金
T.A.科罗达耶娃;A.P.夏什金
..............page:73-78
Testing Investigation for Round Jet with PDPA System
Zhang Weizhi;Zhang Shoujun;Wang Dan
Zhang Weizhi;Zhang Shoujun;Wang Dan
..............page:66-72
An Experimental Study of the Wind Load[1〗on the Huge Roof of An Athletic Ground
Du Xiangdong;Meng Xianzhong;Niu Zhennan;Zhang Boyin;Qian Jihong;Zhao Jida;Zhang Weiyu;Song Tao;Hong Yong
Du Xiangdong;Meng Xianzhong;Niu Zhennan;Zhang Boyin;Qian Jihong;Zhao Jida;Zhang Weiyu;Song Tao;Hong Yong
..............page:58-65
Wall Interference Correction Method for Wind-tunnel[1〗Experiments of Aircraft Model with Propeller
Ni Zhangsong;He Dexin
Ni Zhangsong;He Dexin
..............page:50-57
Wind-Tunnel Investigation of Nose Strakes for Improvement of Lateral and Directional Aerodynamic Characteristics at High Angle of Attack
Zhu Minghong;Wang Xunnian;Chen Hong
Zhu Minghong;Wang Xunnian;Chen Hong
..............page:44-49
A Test Research in Wind Tunnel for Aerodynamic Loads Effect on Separation Trajectories of The Internal Missile of Fighter
Wang Xunnian;Li Jun;Liu Xiaohui
Wang Xunnian;Li Jun;Liu Xiaohui
..............page:38-43
The Experimental Investigation on Reynolds Number Effects on Aerodynamics Data of Fighter Models in Wind Tunnels at High Angles of Attack
Cheng Houmei;Yang Ximing;Sun Shaopeng
Cheng Houmei;Yang Ximing;Sun Shaopeng
..............page:30-37
An Investigation of Basic Behaviour of Atomization[1〗Region Formed by Secondary Breakup of Liquid Ring
Cai Qingjun;Han Zhaoyuan;Wan Qun;Zhang Shouqi
Cai Qingjun;Han Zhaoyuan;Wan Qun;Zhang Shouqi
..............page:22-29
The Effect of Interaction of Shock Waves with Boundary Layers to The Cold Internal Flow Field of A Dual-Combustor Scramjet Model
Zhang Shudao;Han Zhaoyuan;Xu Shengli;Situ Ming
Zhang Shudao;Han Zhaoyuan;Xu Shengli;Situ Ming
..............page:16-21
A Method to Determine Block Coefficient from Test Loss Coefficient
Xing Xiuqing;Zhang Jian;Zhou Sheng
Xing Xiuqing;Zhang Jian;Zhou Sheng
..............page:10-15
Development of the oil film method of skin friction measurement for curved and free oriented surfaces
R.V.内斯塔娅;S.B.尼基弗罗夫;A.A.帕夫洛夫
R.V.内斯塔娅;S.B.尼基弗罗夫;A.A.帕夫洛夫
..............page:1-9