New Magnetic Field Setup for Electromagnetic Flow Control of Lifting Reentry Vehicle
Author:
Affiliation:
1. Department of Mechanical and Systems Engineering, Ryukoku University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/16/7/16_588/_pdf
Reference13 articles.
1. 1) Fujino, T., Sugita, H., Mizuno, M., Funaki, I., and Ishikawa, M.: Influences of Electrical Conductivity of Wall on Magnetohydrodynamic Control of Aerodynamic Heating, J. Spacecraft Rockets, 43 (2006), pp.63-70.
2. 2) Otsu, H., Konigorski, D., and Abe, T.: Influence of Hall Effect on Electrodynamic Heat Shield System for Reentry Vehicles, AIAA J., 48 (2010), pp. 2177-2186.
3. 3) Katsurayama, H., Abe, T., Otsu, H., and Konigorski, D.: Numerical Study of the Electromagnetic Control of a Weakly Ionized Flow Around a Blunt Body: Role of a Insulative Boundary in the Flow,AIAA Paper 2007-4529, 2007.
4. 4) Otsu, H., Matsuda, A., Abe, T., and Konigorski, D.: Numerical Validation of the Magnetic Flow Control for Reentry Vehicles, AIAA Paper 2006-3236, 2006.
5. 5) Matsuda, A., Wakatsuki, K., Takizawa, Y., Kawamura, M., Otsu, H.,Konigorski, D., Sato, S., and Abe, T.: Shock Layer Enhancement by Electro-magnetic Effect for Spherical Blunt Body, AIAA Paper 2006- 3236, 2006.
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