Abstract
The presented work discusses the implementation, verification, and validation of Park’s two-temperature model in a scalable, computational fluid dynamics (CFD) code developed at the US Department of Energy’s Oak Ridge National Laboratory (ORNL). The implementation of Park’s two-temperature model was verified through 0D test cases involving an adiabatic reactor and a nitrogen thermal bath. The implementation was then validated through comparisons with other validated CFD codes and experimental data on a hypersonic cylinder and double cones. These are standard benchmark test cases for thermochemical non-equilibrium (TCNE) modeling, and all data are shared publicly. The verification and validation results showed that ORNL’s in-house CFD code could model complex, high-speed flow problems with and without TCNE modeling. This work is essential for future research involving 3D shock wave/boundary layer interactions (SBLIs).∗
Original language | English |
---|---|
Title of host publication | AIAA Aviation Forum and ASCEND, 2024 |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624107160 |
DOIs | |
State | Published - 2024 |
Event | AIAA Aviation Forum and ASCEND, 2024 - Las Vegas, United States Duration: Jul 29 2024 → Aug 2 2024 |
Publication series
Name | AIAA Aviation Forum and ASCEND, 2024 |
---|
Conference
Conference | AIAA Aviation Forum and ASCEND, 2024 |
---|---|
Country/Territory | United States |
City | Las Vegas |
Period | 07/29/24 → 08/2/24 |
Funding
The authors acknowledge the financial support of the US Department of Energy (DOE) and UT\u2013Battelle, LLC.