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Nonlinear development of crossflow vorticesNonlinear crossflow vortices in an incompressible three-dimensional boundary layer are computed by weakly nonlinear theory and direct numerical simulations. The parallel basic flow is defined by Falkner-Skan-Cooke similarity profiles. The temporal evolution of spanwise periodic, quasi-two-dimensional disturbances without variations along the vortex axis is considered. The nonlinear theory is based on the approach of Herbert (1980, 1983). The theory predicts the existence of the finite amplitude equilibrium states seen in earlier simulations. When the disturbance amplitudes are small, there is very good quantitative agreement in the fundamental disturbance velocity components between the theory and the simulations.
Document ID
19910046730
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Singer, Bart A.
(High Technology Corp. Hampton, VA, United States)
Meyer, F.
(High Technology Corp. Hampton, VA, United States)
Kleiser, Leonhard
(DLR, Institut fuer theoretische Stroemungsmechanik, Goettingen Federal Republic of Germany, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aerodynamics
Meeting Information
Meeting: Instability and Transition
Location: Hampton, VA
Country: United States
Start Date: May 15, 1989
End Date: June 9, 1989
Sponsors: ICAS, NASA
Accession Number
91A31353
Funding Number(s)
CONTRACT_GRANT: NAS1-18240
CONTRACT_GRANT: NAS1-18605
Distribution Limits
Public
Copyright
Other

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