Numerical simulation of the interaction between weak shock waves and supersonic boundary layer on a flat plate with the blunt leading edge
The interaction of weak shock waves in form of an N-wave with the supersonic laminar boundary layer on a flat plate with blunt leading edge at the free-stream Mach number M = 2.5 is numerically studied. The numerical results are compared with known experimental data. The combined influence of the N-wave and the leading edge bluntness on the laminar-turbulent transition process is discussed.
Authors
- Н. К. Нгуен
- P. V. Chuvakhov (ORCID: https://orcid.org/0000-0002-5189-9074)
- И. В. Егоров (ORCID: https://orcid.org/0000-0003-1190-9941)
Institutions
- Moscow Institute of Physics and Technology (RU)
- Central Aerohydrodynamic Institute (RU)
Publication Details
- Journal
- Известия Российской академии наук Механика жидкости и газа
- Published
- 2024-10-19
- DOI
- https://doi.org/10.31857/s1024708424020102
- Primary Topic
- Computational Fluid Dynamics and Aerodynamics
- Type
- article
- Field-Weighted Citation Impact
- 0.00