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Aerodynamic Analysis Methods for Advanced Space Launchers. Limited Survey

机译：先进空间发射器的空气动力学分析方法。有限的调查

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In the report, the development of an analytical calculation procedure for thedetermination of the subsonic aerodynamic characteristics of a space launcher is presented. Also, a first assessment of several methods for Computational Fluid Dynamics.

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作者
Pagen, M. J.;
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年度 1993
页码 p.1-62
总页数 62
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Air launching; Aerospaceplanes; Subsonic flow; Aerodynamic heating; Aerothermodynamics; Computational fluid dynamics;

机译：空气发射;航空航天飞机;亚音速流动;空气动力学加热;气动热力学;计算流体动力学;

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Aerodynamic Analysis Methods for Advanced Space Launchers. Limited Survey

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