Analysis of dynamic stability and numerical computtion of dynamic stability derivative coefficient for reentry aircraft

机译：再入飞行器动态稳定性分析及动态稳定性导数的数值计算。

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This paper presented numerical computation of the dynamic stability derivative coefficient for two typical reentry aircraftu0014u0014the simplified Colombia space shuttle orbiter (life mode) and the spaceship command module (trajectory-life mode), under subsonic, transonic and supersonic speeds.

机译：本文介绍了两种典型的再入飞机在亚音速，跨音速和超音速速度下的动态稳定性微分系数的数值计算，这是简化的哥伦比亚航天飞机的轨道飞行器（生命模式）和宇宙飞船的命令模块（轨迹-生命模式）。

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《Proceedings of The Fourth Asian Computational Fluid Dynamics Conference September 18-22, 2000 Mianyang, China Edited by Zhang Hanxin》|2000年|p.635-640|共6页
会议地点 Mianyang(CN);Mianyang(CN)
作者
Luo Jianguo; Zhang Jianbai;
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原文格式 PDF
正文语种 eng
中图分类力学;
关键词
Space shuttle orbiter, Spaceship command module, Unsteady flow Numerical method, Dynamic stability derivative coefficient;

机译：航天飞机轨道器，飞船指令模块，非恒定流数值方法，动态稳定性导数系数;

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4. Analysis of dynamic stability and numerical computtion of dynamic stability derivative coefficient for reentry aircraft [C] . Luo Jianguo, Zhang Jianbai Asian computational fluid dynamics conference . 2000

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Analysis of dynamic stability and numerical computtion of dynamic stability derivative coefficient for reentry aircraft

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