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Convective heating of small-radius spherical blunting for relatively low hypersonic velocities

  • Heat and Mass Transfer and Physical Gasdynamics
  • Published:
High Temperature Aims and scope

Abstract

The chemically and thermally nonequilibrium air flow over a spherically blunted cylinder for velocities within M = 6–18 with free-stream parameters corresponding to the altitudes of 22 and 37 km is considered. The cylinder bluntness radius is varied within R n = 0.66–5.08 cm. The initial data are chosen on the basis of a series of experimental data on convective heating of the leading critical point of spherical bluntness. These experimental data are in good agreement with the results of numerical simulation.

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Authors and Affiliations

  1. Institute for Problems in Mechanics, Russian Academy of Sciences, pr. Vernandskogo 101-1, 119526, Moscow, Russia

    S. T. Surzhikov

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  1. S. T. Surzhikov
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Original Russian Text © S.T. Surzhikov, 2013, published in Teplofizika Vysokikh Temperatur, 2013, Vol. 51, No. 2, pp. 261–276.

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Surzhikov, S.T. Convective heating of small-radius spherical blunting for relatively low hypersonic velocities. High Temp 51, 231–245 (2013). https://doi.org/10.1134/S0018151X13010185

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  • DOI: https://doi.org/10.1134/S0018151X13010185

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