Particle Computations of Hypersonic Shock Interaction Flows
Final technical rept. 1 Nov 2000-31 Dec 2003
MICHIGAN UNIV ANN ARBOR DEPT OF AEROSPACE ENGINEERING
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Development is described of a hybrid DSMCCFD code for physically accurate and numerically efficient computation of hypersonic, viscous-interaction flows. Recent studies focus on the application and assessment of a hybrid code to a blunted cone configuration and to improvement of physical models used in the code.
- Fluid Mechanics