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A Numerical and Experimental Investigation of Flow Separation Control over a Wall-Mounted Hump ModelNumerical simulations and wind tunnel experiments were performed to investigate flow separation and its control over a wall-mounted hump model. Three-dimensional, unsteady fluid dynamic simulations were used to capture the relevant flow physics of unsteady flow separation and its control via active and passive flow control methods. Surface pressure measurements and surface oilflow visualization were obtained in the experiments. Current measurements documented a considerably thinner incoming boundary layer, but similar pressure distribution, compared to the reference data reported in the CFD (Computational Fluid Dynamics) Validation (CFDVAL 2004) Experiments. Consistent with the data available in the literature, numerical simulations predicted a longer separation bubble, which manifested itself as a shift in the pressure distributions. Streamwise vortices generated by passive vortex generators increased the suction pressure and provided substantial pressure recovery. Numerical simulations of vortex generators qualitatively predicted the effects of control, and revealed patterns of attached/separated flow regions. On the other hand, active flow control using steady discrete jets reduced, but was not able to eliminate, flow separation for the tested configuration. Although the major disagreement between the numerical and experimental results was in the pressure recovery region due to the inaccurate prediction of separation bubbles, the relative pressure recoveries from the baselines were comparable. Surface oilflow visualization and simulated surface streamlines were qualitatively in good agreement revealing the key flow features.
Document ID
20180006299
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Koklu, Mehti
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
October 16, 2018
Publication Date
January 8, 2018
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-28905
Report Number: NF1676L-28905
Funding Number(s)
WBS: WBS 081876.02.07.02.01.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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