Ram-Scram Transition and Flame/Shock-Train Interactions in a Model Scramjet Experiment

By M. Fotia, J. Driscoll. 2013

148 citations recorded by the source corpus.

Subfields: Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/c85e8ad93e92a9c091f9a6af81d525ab6528c68c

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In Computational Mechanics

1. Hong-bo Wang
2. Mingbo Sun
3. Zhenguo Wang

Citations in the corpus

• Review of cavity-stabilized combustion for scramjet applications (2014, background): “Flow or flame unsteadiness, such as turbulence, flow separation, shock waves, shock/boundary-layer or flow/flame interactions, may also introduce significant oscillations to the supersonic combustion systems under certain conditions.(9,41,71,72,77)”