Aerodynamics of indirect thrust measurement by the impulse method

被引：0
|
作者：
Cheng-Kang Wu
Hai-Xing Wang
Xian Meng
Xi Chen
Wen-Xia Pan
机构：
[1] Chinese Academy of Sciences,Institute of Mechanics
[2] Beijing University of Aeronautics and Astronautics,School of Astronautics
[3] Tsinghua University,Department of Engineering Mechanics
来源：
Acta Mechanica Sinica | 2011年 / 27卷
关键词：
Thrust measurement; Impulse method; Aerodynamic features; Cold jet; Arc-heated jet;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The aerodynamic aspects of indirect thrust measurement by the impulse method have been studied both experimentally and numerically. The underlying basic aerodynamic principle is outlined, the phenomena in subsonic, supersonic and arc-heated jets are explored, and factors affecting the accuracy of the method are studied and discussed. Results show that the impulse method is reliable for indirect thrust measurement if certain basic requirements are met, and a simple guideline for its proper application is given.
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收藏
页码：152 / 163
页数：11
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