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High Temperature

, Volume 43, Issue 5, pp 733–745 | Cite as

Aerodynamic Heating of a Thin Sharp-Nose Circular Cone in Supersonic Flow

  • V. A. Bashkin
  • I. V. Egorov
  • V. V. Pafnut'ev
Heat and Mass Transfer and Physical Gasdynamics

Abstract

The assumption of flow symmetry is made to investigate a supersonic flow (M = 5) past a thin circular cone with a half-angle θ c = 4° and an isothermal surface (T w0 = 0.5) by way of numerical integration of unsteady-state three-dimensional Navier-Stokes and Reynolds equations. The calculations are performed in a discrete range of variation of the Reynolds number (104 ≤ Re ≤ 108) and angle of attack (0° ≤ α ≤ 15°). The effect of the determining parameters of the problem on the structure of flow field and on aerodynamic heating of the body surface subjected to flow is demonstrated.

Keywords

Physical Chemistry Reynolds Number Flow Field Body Surface Plasma Physics 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer Science+Business Media, Inc. 2005

Authors and Affiliations

  • V. A. Bashkin
    • 1
  • I. V. Egorov
    • 1
  • V. V. Pafnut'ev
    • 1
  1. 1.N.E. Zhukovskii Central Institute of Aerohydrodynamics (TsAGI)Zhukovskii, Moscow oblastRussia

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