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DSMC Simulations of Hypersonic Flows and Comparison With ExperimentsThis paper presents computational results obtained with the direct simulation Monte Carlo (DSMC) method for several biconic test cases in which shock interactions and flow separation-reattachment are key features of the flow. Recent ground-based experiments have been performed for several biconic configurations, and surface heating rate and pressure measurements have been proposed for code validation studies. The present focus is to expand on the current validating activities for a relatively new DSMC code called DS2V that Bird (second author) has developed. Comparisons with experiments and other computations help clarify the agreement currently being achieved between computations and experiments and to identify the range of measurement variability of the proposed validation data when benchmarked with respect to the current computations. For the test cases with significant vibrational nonequilibrium, the effect of the vibrational energy surface accommodation on heating and other quantities is demonstrated.
Document ID
20040085340
Document Type
Other
Authors
Moss, James N. (NASA Langley Research Center Hampton, VA, United States)
Bird, Graeme A. (GAB Consulting Proprietary Ltd. Sydney, Australia)
Markelov, Gennady N. (AOES Leiden)
Date Acquired
August 21, 2013
Publication Date
July 6, 2004
Subject Category
Fluid Mechanics and Thermodynamics
Meeting Information
24th International Symposium on Rarefied Gas Dynamics(Bari)
Distribution Limits
Public
Copyright
Public Use Permitted.

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