Thermal Protection with Opposing Jet in High Enthalpy Flow
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyushu University
2. Department of Aeronautics and Astronautics, Kyushu University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/astj/15/0/15_JSASS-D-15-00073/_pdf
Reference23 articles.
1. 1) Sivolella, D.: To Orbit and Back Again, How the Space Shuttle Flew in Space, Springer, Chichester, UK, 2014.
2. 2) Fay, J. A. and Riddell, F. R.: Theory of Stagnation Point Heat Transfer in Dissociated Air, J. Aeronautical Sciences, 25 (1958), pp. 73-85, p.121.
3. 3) Walberg, G. D.: A Survey of Aeroassisted Orbit Transfer, J. Spacecraft, 22 (1985), pp. 3-18.
4. 4) Huang, W.: A Survey of Drag and Heat Reduction in Supersonic Flows by a Counterflowing Jet and Its Combinations, J. Zhejiang Univ-Sci A (Appl Phys & Eng), 16 (2015), pp. 551-561.
5. Numerical Analysis of the Piston Motion in a Free Piston Driver
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