Abstract
We investigate adaptive finite element methods for low Mach, steady, laminar combustion. The finite element discretization of the flame equations involves least squares control of streamline derivatives and pressure-velocity coupling as well as a new shock capturing term based on nonlinear crosswind diffusion yielding a suitable discrete maximum principle for the discrete solution. A posteriori error estimates derived from the dual weighted residual method are used to refine the mesh adaptively. Numerical results are presented for a Bunsen flame with simple chemistry on locally refined as well as fully unstructured Delaunay meshes. Solution quality is evaluated in terms of overall flame characteristics - including length, lift off and width - as well as undershoots in species and temperature profiles.
| Original language | English |
|---|---|
| Pages (from-to) | 472-492 |
| Number of pages | 21 |
| Journal | Journal of Computational Physics |
| Volume | 188 |
| Issue number | 2 |
| DOIs | |
| Publication status | Published - 1 Jul 2003 |
Keywords
- A posteriori error estimation
- Adaptive mesh refinement
- Combustion
- Crosswind diffusion
- Finite elements
- Shock capturing
Fingerprint
Dive into the research topics of 'An adaptive finite element method with crosswind diffusion for low Mach, steady, laminar combustion'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver