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Direct Simulation of Reentry Flows with IonizationThe Direct Simulation Monte Carlo (DSMC) method is applied in this paper to the study of rarefied, hypersonic, reentry flows. The assumptions and simplifications involved with the treatment of ionization, free electrons and the electric field are investigated. A new method is presented for the calculation of the electric field and handling of charged particles with DSMC. In addition, a two-step model for electron impact ionization is implemented. The flow field representing a 10 km/sec shock at an altitude of 65 km is calculated. The effects of the new modeling techniques on the calculation results are presented and discussed.
Document ID
20040129606
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Carlson, Ann B.
(NASA Langley Research Center Hampton, VA, United States)
Hassan, H. A.
(North Carolina State Univ. Raleigh, NC, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1989
Subject Category
Fluid Mechanics And Thermodynamics
Funding Number(s)
CONTRACT_GRANT: NAGW-1331
CONTRACT_GRANT: NAGW-1022
CONTRACT_GRANT: NCC1-112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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