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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Bibliographic Details
Published in:AIAA journal 1998-11, Vol.36 (11), p.1983-1990
Main Authors: Spyropoulos, Evangelos T, Blaisdell, Gregory A
Format: Article
Language:English
Subjects:
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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Description
Summary: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