The high-temperature environment poses an unusual challenge in understanding the basic physics of hypersonic flight. A lack of such understanding can lead to risks and uncertainties in the design of aerospace vehicles. Hypersonic Nonequilibrium Flows documents recent, unprecedented scientific advances in the field of nonequilibrium processes for aerospace applications. These advances have been driven primarily by interest in space access and exploration, or in developing military technologies involving hypersonic flight regimes.
Computation of Hypersonic Nonequilibrium Flows using the Direct Simulation Monte Carlo Method
2015-01-01
58 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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