Laminar-Turbulent Transition Behind Discrete Roughness Elements in a High-Speed Boundary Layer

Computations are performed to study the flow past an isolated roughness element in a Mach 3.5, laminar, flat plate boundary layer. To determine the effects of the roughness element on the location of laminar-turbulent transition inside the boundary layer, the instability characteristics of the stati...

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Bibliographische Detailangaben

Hauptverfasser:	Choudhari, Meelan M., Li, Fei, Wu, Minwei, Chang, Chau-Lyan, Edwards, Jack R., Jr, Kegerise, Michael, King, Rudolph
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamics
Online-Zugang:	Volltext bestellen
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