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Computation of a Synthetic Jet in a Turbulent Cross-Flow Boundary LayerA series of unsteady Reynolds-averaged Navier-Stokes computations are performed for the flow of a synthetic jet issuing into a turbulent boundary layer through a circular orifice. This is one of the validation test cases from a synthetic jet validation workshop held in March 2004. Several numerical parameters are investigated, and the effects of three different turbulence models are explored. Both long-time-averaged and time-dependent phase-averaged results are compared to experiment. On the whole, qualitative comparisons of the mean flow quantities are fairly good. There are many differences evident in the quantitative comparisons. The calculations do not exhibit a strong dependence on the type of turbulence model employed.
Document ID
20040152076
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Rumsey, Christopher L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2004
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
L-19052
NASA/TM-2004-213273
Report Number: L-19052
Report Number: NASA/TM-2004-213273
Funding Number(s)
WORK_UNIT: WU 23-762-45-MF
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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