DSMC Simulations of Hypersonic Flows with Shock Interactions and Validation with Experiments-Reference-Cited by-同舟云学术

DSMC Simulations of Hypersonic Flows with Shock Interactions and Validation with Experiments

Published:2004-06-20 Issue: Volume: Page:
ISSN:
Container-title:37th AIAA Thermophysics Conference
language:
Short-container-title:

Author:

Moss James¹,Bird Graeme²

Affiliation:

1. NASA Langley Research Center

2. G.A.B. Consulting Pty Ltd

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2585

Reference18 articles.

1. Marini,Marco,\AReviewofShock-WaveBoundary-Layer LaminarInteractionsonSharpLeadingEdgeRampCon gurations,"ECCOMAS2000Paper,Barcelona,Spain,Sept.2000.

2. Knight,D.\RTOWG10: TestCasesforCFDValidation ofHypersonicFlight,"AIAAPaper2002-0433,January2002.

3. Walker, S., and Schmisseur, J. D. \CFD Validation of Shock-Shock Interaction FlowFields,"AIAAPaper2002-0436, January2002.

4. Bird,G.A.,MolecularGasDynamicsandtheDirectSimulation of Gas Flows. Oxford: ClarendonPress,1994.

5. Bird,G.A.,Visual DSMCProgram forTwo-Dimensional and Axially Symmetric Flows. The DS2V Program User's Guide,Version2.1,November2003.

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