High-order shock-fitting methods for direct numerical simulation of hypersonic flow with chemical and thermal nonequilibrium-Reference-Cited by-同舟云学术

High-order shock-fitting methods for direct numerical simulation of hypersonic flow with chemical and thermal nonequilibrium

Published:2011-09 Issue:23 Volume:230 Page:8474-8507
ISSN:0021-9991
Container-title:Journal of Computational Physics
language:en
Short-container-title:Journal of Computational Physics

Author:

Prakash A.,Parsons N.,Wang X.,Zhong X.

Publisher

Elsevier BV

Subject

Computer Science Applications,Physics and Astronomy (miscellaneous),Applied Mathematics,Computational Mathematics,Modelling and Simulation,Numerical Analysis

Reference70 articles.

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2. F.G. Blottner, M. Johnson, M. Ellis, Chemically Reacting Viscous Flow Program for Multi-Component Gas Mixtures, Report No. SC-RR-70-754, Sandia Laboratories, Albuquerque, New Mexico.

3. Critical hypersonic aerothermodynamic phenomenon;Bertin;Annual Review of Fluid Mechanics,2006

4. G.V. Candler, The Computation of Weakly Ionized Hypersonic Flows in Thermochemical Nonequilibrium, Ph.D. Thesis, June 1988.

5. F.M. Cheatwood, P.A. Gnoffo, Users Manual for the Langley Aerothermal Upwind Relaxation Algorithm (LAURA), NASA TM-4674, April 1996.

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