Turbulence Model Implementation and Verification in the SENSEI CFD CodeThis paper outlines the implementation and verification of the negative Spalart-Allmaras turbulence model into the SENSEI CFD code. The SA-neg turbulence model is implemented in a flexible, object-oriented framework where additional turbulence models can be easily added. In addition to outlining the new turbulence modeling framework in SENSEI, an overview of the other general improvements to SENSEI is provided. The results for four 2D test cases are compared to results from CFL3D and FUN3D to verify that the turbulence models are implemented properly. Several differences in the results from SENSEI, CFL3D, and FUN3D are identified and are attributed to differences in the implementation and discretization order of the boundary conditions as well as the order of discretization of the turbulence model. When a solid surface is located near or intersects an inflow or outflow boundary, higher order boundary conditions should be used to limit their effect on the forces on the surface. When the turbulence equations are discretized using second order spatial accuracy, the edge of the eddy viscosity profile seems to be sharper than when a first order discretization is used. However, the discretization order of the turbulence equation does not have a significant impact on output quantities of interest, such as pressure and viscous drag, for the cases studied.
Document ID
20200002666
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Jackson, Charles W. (NASA Langley Research Center Hampton, VA, United States)
Tyson, William C. (Virginia Tech Blacksburg, VA, United States)
Roy, Christopher J. (Virginia Tech Blacksburg, VA, United States)
Date Acquired
April 17, 2020
Publication Date
January 7, 2019
Subject Category
AerodynamicsMathematical And Computer Sciences (General)
Report/Patent Number
NF1676L-31835Report Number: NF1676L-31835
Meeting Information
Meeting: SciTech 2019
Location: San Diego, CA
Country: United States
Start Date: January 7, 2019
End Date: January 11, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)