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TURBULENCE MODEL NUMERICAL ANALYSIS
2D Finite Flat Plate Validation Case
This case is designed primarily for numerical
analysis of turbulence model simulations; e.g., convergence properties, effect of order of accuracy, etc.
Note that the grids and definition of this case have been changed as of 10/02/2014.
The purpose here is to provide a validation
case for turbulence models similar to the earlier Flat Plate Verification
case, except that the grid extends both upstream and downstream of the plate.
This eliminates possible issues associated with prescribing pressure at the trailing edge of the plate.
A large sequence of nested grids
of the same family are provided here if desired. The data for comparison for this
"essentially incompressible" flat plate case are from theory and correspond to the same
data used for the earlier
Flat Plate Verification case.
The boundary conditions and flow conditions are similar to the earlier case. The turbulent flat plate case should be run at
essentially incompressible conditions (M = 0.2 here).
For the grids given below, running at a Reynolds number per unit length of Re = 5 million
is sufficient to achieve desired Retheta levels.
The following plot shows the layout of the finite
flat plate grids, along with typical boundary conditions.
What to Expect:
(Other turbulence model results may be added in the future.)
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Responsible NASA Official:
Ethan Vogel
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Clark Pederson
Last Updated: 07/21/2016