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Axisymmetric Shock Wave Boundary Layer Interaction near M=7 Validation Case
k-e-Rt Model Results
Link to k-e-Rt equations
Note that thorough
grid studies were not performed for validation cases such as this one.
Some effort was made to ensure reasonable grid resolutions, but there may still be
small noticeable discretization errors. Therefore, these validation results shown should be considered
representative, but not "truth."
The plots shown compare the k-e-Rt results from CFD++,
along with experimental data.
CFD++ used freestream turbulence intensity=0.5% and freestream turbulent viscosity (relative to laminar)=30.
Please read note 5 on Notes on running CFD page.
These results are from the second-finest grid (161x201; 161x201).
Note that for these runs,
no specific turbulence model compressibility corrections have been employed.
Note that this model is currently assigned
MRR Level 1 for the purposes of this website.
This is because at this time the TMBWG has results for this model
from only one code. The results on this page are therefore not necessarily
reliable until additional independent code(s) can be used to verify the model implementation.
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Responsible NASA Official:
Ethan Vogel
Page Curator:
Clark Pederson
Last Updated: 08/28/2020