| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8059114 | Progress in Aerospace Sciences | 2012 | 8 Pages |
Abstract
⺠Hypersonic flow calculations require velocity slip and temperature jump conditions at surfaces. ⺠Patterson's boundary conditions are available, as well as the Maxwell/Smoluchowski conditions. ⺠In results of CFD simulations, Patterson's temperature condition outperforms Smoluchowski's.
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Aerospace Engineering
Authors
Christopher J. Greenshields, Jason M. Reese,