An ILES Analysis of TransverseJet Injection into Supersonic Cross-flow with Synthetic Turbulent Boundary Layer

Research output: Contribution to conferencePaperpeer-review

Original languageEnglish
Publication statusPublished - 2011
Event49th AIAA Aerospace Sciences
Meeting including the New Horizons Forum and Aerospace Exposition
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Duration: 4 Jan 20117 Jan 2011

Conference

Conference49th AIAA Aerospace Sciences
Meeting including the New Horizons Forum and Aerospace Exposition
Period4/01/117/01/11

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