LES and Acoustic Analysis of Turbulent Reacting Flows: Application to a 3D Oscillatory Ramjet Combustor (AIAA 2006-0151)
44th, Aerospace sciences meeting: a collection of technical papers, Vol 3 ; 2006 ; Reno, NV
2006-01-01
10 pages
Vol.3 of 23. See also m06/23197-23220
Conference paper
English
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Shock-Induced Mixing Enhancement of Supersonic Turbulent Reacting Ramjet Flows
British Library Conference Proceedings | 1995
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