Estimated accuracy of the analysis of momentum loss thickness in the laminar boundary layer on a hemisphere impermeable surface in a supersonic air flow
Published: 08.10.2014
Authors: Gorskiy V.V., Sysenko V.A.
Published in issue: #10(34)/2014
DOI: 10.18698/2308-6033-2014-10-1245
Category: Mathematic modeling | Chapter: Modeling aerohydrodynamics