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Experiments and Measurements in Fluid Mechanics
1007-3124
1999 Issue 1
The Effect to The Law of Ground Touch Explosion by the Width of Mountain Valley
Cao Wei Cao Shuding Beijing High Technology Information Institution;Beijing 100085
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page:26-31
The Application of Gas Self Luminosity in Hypersonic Flow Field Visualization
Yuan Shengxue Huang Zhicheng Institute of mechanics;Chinese Academy of Sciences;Beijing 100080
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page:60-64
The Construction of 4m×2.2m Test Section for Wind Engineering in 4m×3m Wind Tunnel
Liang Jian Wang Xunnian Chen Hong Liu Yixin China Aerodynamics Research and Development Center;Mianyang 621000
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page:44-49
Flow Field Measurement of The Reduced Space Shuttle Model
Wang Chensheng Zhang Hongwei Shenyang Aerodynamics Research Institute;Shenyang 110034
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page:78-86
The Development of 96 Test System for Measuring Dynamic Derivatives at High Angle of Attack
Sun Haisheng China Aerodynamics Research and Development Center;Mianyang 621000
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page:32-38
Studies on Hydrogen/Air Supersonic Combustion
Yu Gang Li Jianguo Laboratory of High Temperature Gas Dynamics Institute of Mechanics;Chinese Academy of Science;Beijing 100080
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page:2-13
Investigation of Pedestrian Level Wind Around A High Rise Building with Wind Tunnel Simulation
Wang Xunnian Zhang Dakong Li Zhenchu Liu Xiaohui China Aerodynamic Research and Development Center;Mianyang 621000
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page:55-59
Development of Small Rolling Moment Measurement Technique
Yang Yingchen Beijing Institute of Aerodynamics;Beijing 100074
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page:74-77
A Study of Experimental Technology for Ejection Seat at High Angles of Attack and High Angles of Side-slip in the High Speed Wind Tunnel
Chen Dehua China Aerodynamics Research and Development Center;Mianyang 621000
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page:50-54
Aeroelastic Model and The Buffet Experimental Technique
Bai Kui Feng Mingxi Beijing Institute of Aerodynamics;Beijing 100074
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page:39-43
The Comparative Investigation of The Experiment Results Between PDPA Technology and HW
Zhang Weizhi Wang Dan Zhang Shoujun China Aerodynamics Research & Development Center;Mianyang 621000
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page:87-92
Flow Visualization For An Unconventional Forebody
Yang Qide Ma Mingsheng Yu Tao Hu Handong Zhou Naichun China Aerodynamics Research and Development Center;Mianyang 621000 Zhang Jiaxing Harbin Aerodynamics Research Institute;Harbin 150008
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page:65-68,71-73
Reynolds Number Effect and Correction Methods for Zero Lift Drag of Tactical Missiles
Chen Dehua Zhao Xiehe China Aerodynamics Research and Development Center;Mianyang 621000
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page:93-97
Characteristic Research on the Pipe Flow Under High Intensity Acoustic Field
Xi Baoshu Xu Hongqing Zhou Liwei Shen Xiaochun Dept.of Eng.Mechanics;Tsinghua University
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page:20-25
The Test Technique of Spin for Vertical Wind Tunnel
Li Yongfu Chengdu Aircraft Design Institute;Chengdu 610041
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page:14-19