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