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Large-Eddy Simulation of Boundary Layer Transition on Swept WingsThe large-eddy simulation of the spatial evolution of a stationary crossflow vortex packet in a three-dimensional boundary layer was performed. Although a coarse grid was used (compared to that required by a direct numerical simulation) the essential features of the disturbance evolution, such as the spanwise disturbance spreading and the vortex rollover, were captured accurately. The eddy viscosity became significant only in the late nonlinear stages of the simulation.
Document ID
20040129662
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Huai, Xiaoli
(Maryland Univ. College Park, MD, United States)
Joslin, Ronald D.
(NASA Langley Research Center Hampton, VA, United States)
Piomelli, Ugo
(Maryland Univ. College Park, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1993
Subject Category
Aerodynamics
Funding Number(s)
CONTRACT_GRANT: NAG1-1089
Distribution Limits
Public
Copyright
Public Use Permitted.
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