Application of Electrodynamic Heat Shield System to Super-Orbital Reentry Vehicles
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Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/54/628/54_628_181/_pdf
Reference17 articles.
1. 1) Poggie, J. and Gaitonde, D. V.: Computational Studies of Magnetic Control in Hypersonic Flow, AIAA Paper 2001-0196, 2001.
2. 2) Takizawa, Y., Sato, S., Abe, T. and Konigorski, D.: Electro-Magnetic Effect on Shock Layer Structure in Reentry-Related High-Enthalpy Flow, AIAA Paper 2004-2162, 2004.
3. 3) Takizawa, Y., Matsuda, A., Sato, S., Abe, T. and Konigorski, D.: Experiment on Shock Layer Enhancement by Electro-Magnetic Effect in Reentry-Related High-Enthalpy Flow, AIAA Paper 2005-4786, 2005.
4. 4) MacCormack, R. W.: Evaluation of the Low Magnetic Reynolds Approximation for Aerodynamic Flow Calculations, AIAA Paper 2005-4780, 2005.
5. 5) Fujino, T., Funaki, I., Sugita, H., Mizuno, M. and Ishikawa, M.: Numerical Analyses on Flow Control around Blunt Body “OREX” by Magnetic Field, AIAA Paper 2003-3760, 2003.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Numerical Simulation of MHD Heat Shield with Consideration of Radiative Heating;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2010
2. Possibility of Thermal Protection in Earth Re-entry Flight by MHD Flow Control with Air-Core Circular Magnet;IEEJ Transactions on Electrical and Electronic Engineering;2009-07
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