Abstract
To identify areas for improvement in RANS simulations for hypersonic flows, newly proposed compressible transformations are examined. The transformations are assessed to determine if they accurately collapse DNS data to the incompressible law of the wall and the effect of the transformation on the implied eddy viscosity is evaluated. Because the compressible transformation implies a specific form for the compressible eddy viscosity, an initial modification to the algebraic Baldwin-Lomax turbulence model is proposed as the first step of a new, compressible correction for RANS turbulence models.
| Original language | English (US) |
|---|---|
| Title of host publication | AIAA SciTech Forum 2022 |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624106316 |
| DOIs | |
| State | Published - 2022 |
| Externally published | Yes |
| Event | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, United States Duration: Jan 3 2022 → Jan 7 2022 |
Publication series
| Name | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 |
|---|
Conference
| Conference | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 |
|---|---|
| Country/Territory | United States |
| City | San Diego |
| Period | 1/3/22 → 1/7/22 |
Bibliographical note
Funding Information:This work is supported by the the DoD High Performance Computing Modernization Program (HPCMP) through the Hypersonic Vehicle Simulation Institute (HVSI) under award number FA7000-19-2-0003.
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.