| Issue |
Volume 9, 2017
Progress in Flight Physics
|
|
|---|---|---|
| Page(s) | 409 - 420 | |
| Section | Shock waves | |
| DOI | https://doi.org/10.1051/eucass/2016090409 | |
| Published online | 20 June 2017 | |
Simulation of hypersonic shock wave - laminar boundary layer interactions
Rutgers, The State University of New Jersey New Brunswick, NJ 08903, USA
The capability of the Navier-Stokes equations with a perfect gas model for simulation of hypersonic shock wave - laminar boundary layer interactions is assessed. The configuration is a hollow cylinder flare. The experimental data were obtained by Calspan-University of Buffalo (CUBRC) for total enthalpies ranging from 5.07 to 21.85 MJ/kg. Comparison of the computed and experimental surface pressure and heat transfer is performed and the computed §ow¦eld structure is analyzed.
© The Authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0 (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.