Compressible Boundary-Layer Predictions at High Reynolds Number Using Hybrid LES/RANS Methods
Author(s) -
JungIl Choi,
Jack R. Edwards,
Robert A. Baurle
Publication year - 2009
Publication title -
aiaa journal
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.828
H-Index - 158
eISSN - 1081-0102
pISSN - 0001-1452
DOI - 10.2514/1.41598
Subject(s) - reynolds averaged navier–stokes equations , boundary layer , reynolds number , mechanics , compressibility , airfoil , physics , mathematics , aerospace engineering , computational fluid dynamics , turbulence , engineering
Simulations of compressible boundary-layer flow at three different Reynolds numbers (Re δ = 5.59 × 10 4 , 1.78 × 10 5 , and 1.58 x 10 6 ) are performed using a hybrid large-eddy simulation/Reynolds-averaged Navier-Stokes method. Variations in the recycling/rescaling method, the higher order extension, the choice of primitive variables, the Reynolds-averaged Navier-Stokes to large eddy simulation transition parameters, and the mesh resolution are considered in order to assess the model. The results indicate that the present model can provide good predictions of the mean-flow properties, second-moment statistics, and structural features of the boundary layers considered. Normalized turbulent statistics in the outer layer are found to be independent of Reynolds number, similar to incompressible turbulent boundary layers.
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