Studies of combustion effects on near-wall turbulence in supersonic flows by large eddy simulation
Author:
Funder
National Natural Science Foundation of China
National Numerical Wind Tunnel Project
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference60 articles.
1. A century of ramjet propulsion technology evolution;Fry;J. Propuls. Power,2004
2. Physics and regimes of supersonic combustion;Ingenito;AIAA J.,2010
3. Turbulent Combustion;Peters,2000
4. A quadrature-based les/transported probability density function approach for modeling supersonic combustion;Koo;Proc. Combust. Inst.,2011
5. Subgrid mixing and molecular transport modeling in a reacting shear layer;Menon;Symp., Int., Combust.,1996
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