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- W44962802 abstract "A review of recent calculations obtained with Bird's direct simulation Monte Carlo (DSMC) method is presented for the transitional flowfield encountered at reentry conditions. Consequently, the emphasis is the real-gas effects resulting from a highly energetic nonequilibrium flow. The DSMC calculations for both wide-angle and slender bodies are compared with continuum calculations. The wide-angle body calculations simulate the windward nose of the Shuttle Orbiter and projected aeroassisted orbital transfer vehicles. For the slender, blunted configurations, both two-dimensional and axisymmetric results are presented. Comparisons between the DSMC and continuum calculations show the altitude range where differences in flowfield structure and surface quantities become significant." @default.
- W44962802 created "2016-06-24" @default.
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- W44962802 date "1986-10-01" @default.
- W44962802 modified "2023-09-27" @default.
- W44962802 title "Numerical simulations of rarefied reentry flows" @default.
- W44962802 hasPublicationYear "1986" @default.
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