Open AccessNumerical study of unsteady effects in the interaction of an incident shock with the transitional boundary layer on a flat plate
Author(s) -
D. V. Khotyanovsky,
A. N. Kudryavtsev
Publication year - 2018
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.5065357
Subject(s) - boundary layer , shock wave , oblique shock , supersonic speed , mach number , mechanics , mach wave , shock (circulatory) , laminar flow , blasius boundary layer , flow separation , boundary layer thickness , physics , boundary layer control , turbulence , boundary (topology) , bow shock (aerodynamics) , mathematics , medicine , mathematical analysis
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