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Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence

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Abstract

The influence of the second-approximation effects of laminar boundary layer theory on the heat transfer in three-dimensional hypersonic flow over blunt cones with a large aspect ratio is investigated numerically.

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Authors
  1. E. A. Lipchinskii
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  2. G. A. Tirskii
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  3. S. V. Utyuzhnikov
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Additional information

Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 2, pp. 57–64, March–April, 1995.

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Lipchinskii, E.A., Tirskii, G.A. & Utyuzhnikov, S.V. Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence. Fluid Dyn 30, 204–209 (1995). https://doi.org/10.1007/BF02029831

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  • DOI: https://doi.org/10.1007/BF02029831

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