Numerical Simulation of a 3D Flow Past an Inlet Model
Numerical simulation of a supersonic flow of viscous heat-conducting gas past an inlet model for various Mach numbers (M = 4 and 5) and temperatures of the model surface is carried out on the basis of an unsteady Reynolds averaged Navier–Stokes (URANS) equations system with the Spalart–Allmaras (SA) and Menter (SST) turbulence model. The three-dimensional features of the flow and heat flux’s dependence on the wall temperature are investigated. The simulation results are compared with the experimental data.
Authors
- Ya. V. Khankhasaeva
- Vitaly Evgenyevich Borisov (ORCID: https://orcid.org/0000-0003-4448-7474)
- А. Е. Lutsky (ORCID: https://orcid.org/0000-0002-4442-0571)
- Б. Н. Четверушкин (ORCID: https://orcid.org/0000-0003-1216-5438)
Institutions
- Keldysh Institute of Applied Mathematics (RU)
Publication Details
- Journal
- Mathematical Models and Computer Simulations
- Published
- 2024-10-01
- DOI
- https://doi.org/10.1134/s2070048224700327
- Primary Topic
- Turbomachinery Performance and Optimization
- Type
- article
- Field-Weighted Citation Impact
- 0.00