Control Parameters for Boundary-Layer Instabilities in Unsteady Shock Interactions
This article presents the computation of a set of control parameters for the deterministic prediction of laminar boundary-layer instabilities induced by an imposed unsteady shock interaction. The objective of the study is exploratory in nature by computing a supersonic flight environment for flow ov...
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Format: | Article |
Language: | English |
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MDPI AG
2012-01-01
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Series: | Entropy |
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Online Access: | http://www.mdpi.com/1099-4300/14/2/131/ |