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Simulation of Synthetic Jets in Quiescent Air Using Unsteady Reynolds Averaged Navier-Stokes EquationsWe report research experience in applying an Unsteady Reynolds-Averaged Navier-Stokes (URANS) solver for the prediction of time-dependent flows in the presence of an active flow control device. The configuration under consideration is a synthetic jet created by a single diaphragm piezoelectric actuator in quiescent air. Time-averaged and instantaneous data for this case were obtained at Langley Research Center, using multiple measurement techniques. Computational results for this case using one-equation Spalart-Allmaras and two-equation Menter s turbulence models are presented here along with comparisons with the experimental data. The effect of grid refinement, preconditioning and time-step variation are also examined.
Document ID
20040112027
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Vatsa, Veer N.
(NASA Langley Research Center Hampton, VA, United States)
Turkel, Eli L.
(Tel-Aviv Univ., Ramat-Aviv Tel-Aviv, Israel)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2004-4967
Report Number: AIAA Paper 2004-4967
Meeting Information
Meeting: 22nd AIAA Applied Aerodynamics Conference and Exhibit
Location: Providence, RI
Country: United States
Start Date: August 16, 2004
End Date: August 19, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 762-45-MC
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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