Development of a Thermo-chemical Non-equilibrium Solver for Hypervelocity Flows-Reference-Cited by-同舟云学术

Development of a Thermo-chemical Non-equilibrium Solver for Hypervelocity Flows

Published:2014-12-25 Issue:2 Volume:96 Page:119-134
ISSN:2250-0545
Container-title:Journal of The Institution of Engineers (India): Series C
language:en
Short-container-title:J. Inst. Eng. India Ser. C

Author:

Balasubramanian R.,Anandhanarayanan K.

Publisher

Springer Science and Business Media LLC

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Ocean Engineering,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1007/s40032-014-0166-5.pdf

Reference11 articles.

1. P.A. Gnoffo, R.N. Gupta, J.L. Shinn, Conservation equations and physical models for hypersonic air flows in thermal and chemical nonequilibrium. NASA Technical Paper 2867, Feb 1989.

2. J.W. Lee, Unstructured cartesian-grid methodology for non-equilibrium hypersonic flows. AIAA paper No. 2007–4548, AIAA Thermophysics Conference, Miami, Florida, USA, June 2007.

3. I. Nompelis, G.V. Candler, S.M. Holden, Effect of vibrational nonequilibrium on hypersonic double-cone experiments. AIAA J. 41(11), 2162–2169 (2003)

4. S. Susheel, M. Zaki, S.M. Ruffin, V. Kolobov, R. Arslanbekov, Evaluation of Viscous Flow Solvers with Adaptive Cartesian Meshes for Hypersonic Flows. AIAA paper No. 2011–4035, 42nd AIAA Thermophysics Conference, Honolulu, Hawaii, Jun3 2011

5. X. Wang, X. Zhong, Development and validation of a high-order shock-fitting non-equilibrium flow solver. 49th AIAA Aerospace Sciences Meeting, AIAA 2011-365, Orlando, Florida, 4–7 January 2011

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