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
The momentum loss thickness in the laminar boundary layer is one of its important characteristics, and the question of the accuracy of its calculation from the known formulae has not been satisfactory described in the literature. In this paper, this problem is solved on the basis of systematic numerical calculations of boundary layer equations.
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