Effect of the Clearance between Two Bodies on TSTO Aerodynamic Heating
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/53/622/53_622_503/_pdf
Reference13 articles.
1. 1) 久保田弘敏:将来型宇宙輸送システムの研究開発に向けて,日本航空宇宙学会第35期年会講演会講演集,2004, pp. 119–122.
2. 2) Dulepov, N. P., Lanshin, A. I., Sokolova, O. V. and Tjurikov, E. V.: Propulsion Systems for TSTO Airplane-Accelerators of Different Types, AIAA Paper 2001-1914, 2001.
3. Aerodynamic Interaction between Delta Wing and Hemisphere-Cylinder in Hypersonic Flow
4. Experimental and numerical investigation of convection heat transfer in transpiration cooling
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