Wall Roughness Effects on Combustion Development in Confined Supersonic Flow
Authors:
- 1 January 2021
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 37 (1) , 151-166
Abstract
Reactive and nonreactive Reynolds-averaged Navier–Stokes simulations of hydrogen injection into a confined transverse supersonic flow of vitiated air are conducted. The corresponding conditions wer...Keywords
Funding Information
- Direction Générale de l'Armement (DGA), French Ministry of Defense
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