On the accuracy of engineering methods for calculation of specific heat flow in laminar boundary layer on non-permeable "wall" of hemisphere surface in a supersonic gas flow
Published: 22.10.2015
Authors: Gorskiy V.V., Sysenko V.A., Blokhina A.A.
Published in issue: #6(42)/2015
DOI: 10.18698/2308-6033-2015-6-1412
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts