High supersonic speed aircraft intake design based on the three-dimensional flow along the corner of intersecting wedges
Published: 04.05.2018
Authors: Tolmachev V.I.
Published in issue: #5(77)/2018
DOI: 10.18698/2308-6033-2018-5-1760
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts