Abstract
The streamlining of bodies with catalytic surfaces is investigated within the framework of a model of a hypersonic three-dimensional viscous shock layer.
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É. A. Gershbein, V. S. Shchelin, and S. A. Yunitskii, Kosm, Issled.,23, No. 3, 416–425 (1985).
H. K. Cheng, J. Astronaut. Sci., No. 92, 1–100 (1963).
R. V. Masek, D. Render, and J. A. Forney, “Evaluation of aerodynamic uncertainties for the space shuttle,” AIAA Paper No. 737, New York (1973).
É. A. Gershbein and V. G. Shcherbak, Izv. Akad- Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 134–142 (1987).
V. G. Shcherbak, Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 5, 143–150 (1987).
C. D. Scott, “Catalytic recombination of nitrogen and oxygen on high-temperature reusable insulation,” AIAA Paper No. 1477, New York (1980).
V. V. Lunev, Hypersonic Aerodynamics [in Russian], Moscow (1975).
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 56, No. 2, pp. 298–301, February, 1989.
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Shcherbak, V.G. Calculating convective heat exchange in a hypersonic viscous shock layer. Journal of Engineering Physics 56, 213–216 (1989). https://doi.org/10.1007/BF00870580
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DOI: https://doi.org/10.1007/BF00870580