Proceedings of the 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering 2015

Numerical Investigation on Chemical Equilibrium Slip Flow of High Altitude and Large Mach Number

Authors
Limin Song, Changdong Li, Kai Luo, Song Li, Yuankai Li
Corresponding Author
Limin Song
Available Online December 2015.
DOI
https://doi.org/10.2991/icmmcce-15.2015.115How to use a DOI?
Keywords
hypersonic slip flow; chemical-equilibrium; computational model
Abstract
In the flight of hypersonic near space vehicle from 60km up to 100km high, the influence of real gas effect, rarefied gas effect, and Mach number effect cannot be simulated completely by the ground test. In this paper, the selection of computational model is introduced, and then carried out the numerical research on slip flow field characteristics coupling with chemical-equilibrium effect under large Mach number of high altitude.
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Proceedings
2015 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering
Part of series
Advances in Computer Science Research
Publication Date
December 2015
ISBN
978-94-6252-133-9
DOI
https://doi.org/10.2991/icmmcce-15.2015.115How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - Limin Song
AU  - Changdong Li
AU  - Kai Luo
AU  - Song Li
AU  - Yuankai Li
PY  - 2015/12
DA  - 2015/12
TI  - Numerical Investigation on Chemical Equilibrium Slip Flow of High Altitude and Large Mach Number
BT  - 2015 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering
PB  - Atlantis Press
UR  - https://doi.org/10.2991/icmmcce-15.2015.115
DO  - https://doi.org/10.2991/icmmcce-15.2015.115
ID  - Song2015/12
ER  -