Magneto-Aerodynamic Hypersonics

机译：magneto-aerodynamic Hypersonics

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Favorable interactions of electromagnetic fields and weakly ionized air for flow control have been recognized since the late 1950s. Potential applications of flow control to hypersonic flight vehicles were recently demonstrated by Russian research and concepts. The scientific knowledge base of this interdisciplinary area (i.e., fluid dynamics, electromagnetics, and chemical and thermal nonequilibrium gas dynamics) is extremely sparse. Therefore, controversy and even misunderstandings are abundant in the research community. This report documents the in-house research project that was initiated to develop a validated magneto-aerodynamic hypersonic analysis capability. The project combined experimental and computational simulations of high-speed gas dynamics in order to verify the scientific findings and define the usable scope for practical hypersonic flight. Sponsorship was provided by the U.S. Air Force Research Laboratory's Office of Scientific Research (AFOSR) as part of an Entrepreneurial Research Initiative over the period 3 January 1999 through 30 September 2003.

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作者
Witzeman, F.;
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年度 2003
页码 1-7
总页数 7
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Electromagnetic fields; Air flow; Ionization; Gas dynamics; Nonequilibrium flow; Fluid dynamics; Hypersonic flight; Hypersonic aircraft; Aerodynamics;

机译：电磁场;空气流动;电离;气体动力学;非平衡流动;流体动力学;高超音速飞行;高超音速飞机;空气动力学;

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Magneto-Aerodynamic Hypersonics

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