Abstract
The authors analyze the results of numerical solution of the equations of the three-dimensional thin viscous shock layer over triaxial ellipsoids of different shapes in a flow of supersonic viscous gas, with no symmetry planes.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 58, No. 2, pp 200–206, February, 1990.
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Borodin, A.I., Peigin, S.V. Investigation of the heat transfer laws in a three-dimensional viscous shock layer on blunt bodies at angle of attack and sideslip. Journal of Engineering Physics 58, 145–151 (1990). https://doi.org/10.1007/BF00872837
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DOI: https://doi.org/10.1007/BF00872837