Abstract
Validation and verification represent an important element in the development of a computational code. The aim is establish both confidence in the algorithm and its suitability for the intended purpose. In this paper, a direct simulation Monte Carlo solver, called dsmcFoam, is carefully investigated for its ability to solve low and high speed non-reacting gas flows in simple and complex geometries. The test cases are: flow over sharp and truncated flat plates, the Mars Pathfinder probe, a micro-channel with heated internal steps, and a simple micro-channel. For all the cases investigated, dsmcFoam demonstrates very good agreement with experimental and numerical data available in the literature.
| Original language | English |
|---|---|
| Pages (from-to) | 140-157 |
| Number of pages | 18 |
| Journal | Computers and Fluids |
| Volume | 120 |
| Early online date | 3 Aug 2015 |
| DOIs | |
| Publication status | Published - 5 Oct 2015 |
Keywords
- aerodynamics
- rarefied gas dynamics
- open-source
- low/high speed flows
- DSMC
- benchmark
Fingerprint
Dive into the research topics of 'Benchmark numerical simulations of rarefied non-reacting gas flows using an open-source DSMC code'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver