A New Calculation Method of Supersonic/Hypersonic Flow
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Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/51/599/51_599_683/_pdf
Reference8 articles.
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2. 2) Nishio, M.: Method for Visualizing Streamline around Hypersonic Vehicles by Using Electric Discharge, AIAA J., 30 (1992), pp. 1662–1663.
3. 3) Dogra, V. K., Moss, J. N. and Price, J. M.: Near-Wake Structure for a Generic Configuration of Aeroassisted Space Transfer Vehicles, J. Spacecraft Rockets, 31 (1994), pp. 953–959.
4. 4) Kim, M. S., Loellbach, J. M. and Lee, K. D.: Effects of Gas Models on Hypersonic Base Flow Calculations, J. Spacecraft Rockets, 31 (1994), pp. 223–230.
5. 5) Dogra, V. K., Taylor, J. C. and Hassan, H. A.: Effects of Chemistry on Blunt-Body Wake Structure, AIAA J., 33 (1995), pp. 463–469.
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1. Flow Patterns around the MESUR Capsule Traveling at Supersonic/Hypersonic Speeds;JSME International Journal Series B;2006
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