Simulations of the SCHOLAR Scramjet Experiment
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition（2012）
Abstract
The DDES method is employed to investigate the complex physics involved in supersonic combustion and in particular in the SCHOLAR scramjet test case. The influence on computational results of prescribing turbulent fluctuations at the entrance to the combustion chamber is investigated. The interaction of shock waves, vortices, turbulence and combustion is studied and the existence of secondary vortices on the upper will of the combustor is proposed. © 2012 by Peter Cocks.
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Key words
scholar,experiment
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