Boundary-layer stability of a generic reentry capsule with real-gas effects
Abstract eng: On the base of a generic Apollo capsule geometry, the present work focuses on the influence of high-temperature gas effects on the flow around the windward side of the blunt body. By means of Direct Numerical Simulations and Linear Stability Analysis, the influence of chemical dissociations and non-equilibrium on the stability of the boundary layer will be investigated.
Publisher:
International Union of Theoretical and Applied Mechanics, 2016
Conference Title:
Conference Title:
24th International Congress of Theoretical and Applied Mechanics
Conference Venue:
Montreal (CA)
Conference Dates:
2016-08-21 / 2016-08-26
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2016-11-15, last modified 2016-11-15
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