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Calculation of turbulent boundary layers with tangential slot injectionPaper describes a numerical calculation scheme for tangential slot injection (wall-wake) flows; application of the scheme over a wide range of flow conditions indicates increased accuracy compared to previous work. Predictions from the numerical code were in good agreement with experiment (velocity profile, skin-friction, and effectiveness data) for low- and high-speed flows. To achieve improved accuracy, modifications in the turbulence modeling, compared to previous research, were necessary for the imbedded shear layer region in the near field and for the wall region near shear layer impingement. Anomalous behavior was noted for far field experimental velocity profiles in low-speed flow when the slot-to-free stream velocity ratio was near one
Document ID
19780049272
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cary, A. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Bushnell, D. M.
(NASA Langley Research Center Hampton, VA, United States)
Hefner, J. N.
(NASA Langley Research Center High-Speed Aerodynamics Div., Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1977
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ASME PAPER 77-WA/HT-29
Meeting Information
Meeting: American Society of Mechanical Engineers, Winter Annual Meeting
Location: Atlanta, GA
Start Date: November 27, 1977
End Date: December 2, 1977
Sponsors: American Society of Mechanical Engineers
Accession Number
78A33181
Distribution Limits
Public
Copyright
Other

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