Development of a Two-Temperature Open-Source CFD Model for Hypersonic Reacting Flows (AIAA 2015-3637)
AIAA international space planes and hypersonic systems and technologies conference
01.01.2015
14 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DataCite | 1915
AIAA-2019-3637: Development of Low Diffusive MLP Limiter for Meshless Method
British Library Conference Proceedings | 2019
|Modeling Hypersonic Reacting Flows Using DSMC with the Bias Reaction Model (AIAA 2017-4025)
British Library Conference Proceedings | 2017
|