Abstract
The aim of this paper is to introduce and validate a coupled Navier-Stokes Boltzman approach for the calculation of hypersonic rarefied flows around manoeuvering vehicles. The proposed strategy uses locally a kinetic model in the boundary layer coupled through wall friction forces to a global Navier-Stokes solver. Different numerical experiments illustrate the potentialities of the method.
| Original language | English |
|---|---|
| Pages (from-to) | 227-245 |
| Number of pages | 19 |
| Journal | Journal of Computational Physics |
| Volume | 127 |
| Issue number | 2 |
| DOIs | |
| Publication status | Published - 1 Jan 1996 |
| Externally published | Yes |