Large-Eddy Simulation of a Spatially Evolving Supersonic Turbulent Boundary-Layer Flow

Several issues involving the large-eddy simulation of wall-bounded compressible turbulent flows are investigated. A spatially evolving supersonic boundary layer is simulated using a high-order-accurate finite difference scheme and the dynamic subgrid-scale model.

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Bibliographische Detailangaben
Veröffentlicht in:	AIAA journal 1998-11, Vol.36 (11), p.1983-1990
Hauptverfasser:	Spyropoulos, Evangelos T, Blaisdell, Gregory A
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Boundary layer and shear turbulence Compressible flow Compressible flows shock and detonation phenomena Computer simulation Energy dissipation Exact sciences and technology Finite difference method Fluid dynamics Fundamental areas of phenomenology (including applications) Physics Simulation Supersonic and hypersonic flows Supersonic flow Turbulence Turbulence simulation and modeling Turbulent flow Turbulent flows, convection, and heat transfer
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Beschreibung
Zusammenfassung:	Several issues involving the large-eddy simulation of wall-bounded compressible turbulent flows are investigated. A spatially evolving supersonic boundary layer is simulated using a high-order-accurate finite difference scheme and the dynamic subgrid-scale model.
ISSN:	0001-1452 1533-385X
DOI:	10.2514/2.325