Abstract
This paper has a dual purpose: it presents a multidomain Chebyshev method for the solution of the two-dimensional reactive compressible Navier–Stokes equations, and it reports the results of the application of this code to the numerical simulations of high Mach number reactive flows in recessed cavity. The computational method utilizes a newly derived interface boundary conditions as well as an adaptive filtering technique to stabilize the computations. The results of the simulations are relevant to recessed cavity flame-holders.
| Original language | English |
|---|---|
| Pages (from-to) | 325-354 |
| Number of pages | 30 |
| Journal | Journal of Computational Physics |
| Volume | 192 |
| Issue number | 1 |
| DOIs | |
| Publication status | Published - 20 Nov 2003 |
User-Defined Keywords
- Multidomain spectral method
- Penalty interface conditions
- Supersonic combustor
- Recessed cavity flame-holder
- Compressible Navier-Stokes equations