Taking into account the vorticity effect in the calculation of the specific heat flow in the laminar boundary layer on hemisphere impermeable surface in a supersonic air flow
Published: 08.10.2014
Authors: Gorskiy V.V., Pugach M.A., Sysenko V.A.
Published in issue: #11(35)/2014
DOI: 10.18698/2308-6033-2014-11-1247
Category: Mathematic modeling | Chapter: Modeling aerohydrodynamics
The analysis of the vorticity effect influence on the specific heat flux in the laminar boundary layer on an impermeable wall at the surface of the hemisphere in a supersonic air flow has been performed. Engineering method is proposed to account for the vorticity effect by correcting the specific heat flux.
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