Appearance of impact starting of the flow in exhaust diffuser used for altitude rocket engine tests
Published: 14.01.2019
Authors: Zakharov V.S., Gouskov O.V., Berezhnoy V.N.
Published in issue: #1(85)/2019
DOI: 10.18698/2308-6033-2019-1-1841
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts