Publication Date:
2019-06-28
Description:
A three-dimensional Navier-Stokes solver was used to determine how accurately computations can predict local and average skin friction coefficients for attached and separated flows for simple experimental geometries. Algebraic and transport equation closures were used to model turbulence. To simulate anisotropic turbulence, the standard two-equation turbulence model was modified by adding nonlinear terms. The effects of both grid density and the turbulence model on the computed flow fields were also investigated and compared with available experimental data for subsonic and supersonic free-stream conditions.
Keywords:
AERODYNAMICS
Type:
NASA-TP-3480
,
L-17354
,
NAS 1.60:3480
Format:
application/pdf
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