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

DOI

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.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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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  - Proceedings of the 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering 2015
PB  - Atlantis Press
SP  - 570
EP  - 574
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmmcce-15.2015.115
DO  - 10.2991/icmmcce-15.2015.115
ID  - Song2015/12
ER  -