Validation of a Novel OpenFOAM Solver using a Supersonic, Non-reacting Channel Flow
19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
2014-01-01
Conference paper
Electronic Resource
English
Validation of a Novel OpenFOAM Solver using a Supersonic, Non-reacting Channel Flow (AIAA 2014-3088)
British Library Conference Proceedings | 2014
|A validation study of OpenFOAM using the supersonic flow in a mixed compression intake
SAGE Publications | 2010
|A validation study of OpenFOAM using the supersonic flow in a mixed compression intake
Online Contents | 2010
|