Interaction of Supersonic Expansion Flow with Boundary Layer in Unsymmetrical Duct.
نویسندگان
چکیده
منابع مشابه
Multi-fidelity numerical simulations of shock/turbulent-boundary-layer interaction in a duct with uncertainty quantification
The interaction between shock waves and turbulent boundary layers (STBLI) plays a fundamental role in the operation of (sc)ramjet engines utilized in supersonic/hypersonic flight vehicles. In particular, the isolator part of such engines is often designed to contain a series of shock waves (shock-train) that sets the flow of incoming, atmospheric air in the optimal conditions for its subsequent...
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ژورنال
عنوان ژورنال: JSME International Journal Series B
سال: 1994
ISSN: 1340-8054,1347-5371
DOI: 10.1299/jsmeb.37.77