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Experimental Verification of CFD Modeling of Turbulent Flow over Circular Cavities using FLUENT University of Western Ontario Department of Mechanical.

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Presentation on theme: "Experimental Verification of CFD Modeling of Turbulent Flow over Circular Cavities using FLUENT University of Western Ontario Department of Mechanical."— Presentation transcript:

1 Experimental Verification of CFD Modeling of Turbulent Flow over Circular Cavities using FLUENT University of Western Ontario Department of Mechanical & Materials Engineering Presented by: Thomas Hering MESc Candidate Advanced Fluid Mechanics Research Group Jesse Dybenko Research Engineer Eric Savory Associate Professor May 23, 2006

2 Overview General overview of experimental parameters CFD grid generation CFD solution procedure Results Key findings Future work (Elliptical Cavities)

3 Background Cavities may lead to increased noise and drag on an object Main focus on Circular cavities: Resulting asymmetric flow and significant increase in drag at h/D ≈ 0.5 h D Flow direction Experimental Variables Side View Top View

4 Experimental Data Collected Three cases of h/D ratio = 0.2, 0.47, 0.7 were tested Pressure transducer data was taken to plot surface pressure contours on cavity walls and surrounding plane Hot Wire anemometry was used to examine the wake flow characteristics The free stream velocity during the experiments was 27 ± 0.15 m/s The pressure coefficient was normalized using the tunnel static pressure and free stream velocity

5 Boundary Conditions and Dimensions The inlet velocity was set to 25 m/s, which resulted in a free stream velocity of 26.4 m/s at the free stream reference point Outflow Wall Velocity Inlet Wall 5.5D 4D 47.3D 32D Cavity Y X Z

6 Simulation Grid Side View Top View Cavity The computation domain was broken up into several volumes which were meshed using a structured hexagonal cooper meshing scheme

7 Solution Procedure Simulated Data Experimental Data The solution was first iterated using the k-ε turbulence model After initial solution convergence the Reynolds Stress model was applied and further iterated The tunnel length was used to develop a similar boundary layer as measured in the experiments A steady state solution sought Boundary Layer Parameters

8 Pressure Distributions P = Pressure P s = Free stream static pressure U o = Free stream velocity = Density of air Pressure Coefficient 0°0° TOP VIEW 90° 180° 270° Cavity sidewall coordinate system Flow direction X Z Due to simulated steady state solution, only the mean values were compared Surface pressure distributions, wake profiles and drag coefficients were compared

9 Pressure Contours for h/D = 0.7 Cavity Side Simulated Experimental Cavity Base SimulatedExperimental Ground Plane SimulatedExperimental 0°0° Flow direction 90° 270° Y X Z Cavity Base Ground Plane 180° Simulated results matched well with experimental data

10 Pressure Distributions along the Centreline for h/D = 0.7 0°0° 90° 270° X Z Centreline used in comparison of cavity side walls 180° Y Flow direction 0° Cavity Wall 180° Cavity Wall Cavity Base Centreline

11 Pressure Contours for h/D = 0.2 Ground Plane ExperimentalSimulated Cavity Base SimulatedExperimental Cavity Side Simulated Experimental Similar trends along the centreline as for the h/D = 0.7 case, but the difference between simulated and experimental data was larger

12 Pressure Contours for h/D = 0.47 (Asymmetric flow) Ground Plane SimulatedExperimental Cavity Base SimulatedExperimental Cavity Side Simulated Experimental Asymmetry is much weaker in the simulated results Vortex tube does not completely leave the cavity in the simulated results

13 Comparison between Turbulence Models for h/D = 0.47 k-ε model Ground Plane Reynolds Stress model Cavity Side k-ε model Reynolds Stress model Cavity Base k-ε modelReynolds Stress model Asymmetry is weaker when applying the k-ε turbulence model

14 Resulting Wake Comparisons h/D = 0.2 Simulated Experimental h/D = 0.47 Simulated Experimental The weak asymmetry can be seen in the wake for h/D = 0.47 case

15 Drag coefficient Comparison C D = Drag coefficient (normalized by the cavity planform area) c f = Skin friction coefficient Experimental drag coefficient calculated using pressure distributions along cavity wall Weaker asymmetry the cause of the lower drag coefficient at h/D = 0.47 Drag increment due to presence of cavity

16 Key Findings The simulated results showed the correct flow physics involved in circular cavity flows The asymmetric flow for a symmetric geometry, a distinct feature of this type of flow, was apparent in the simulations The weaker asymmetry led to a lower drag coefficient The simulations constantly under predicted the pressure values for all three configurations tested The Reynolds Stress Turbulence model provided better results than the k-ε Turbulence model when comparing the strength of the asymmetry at h/D = 0.47

17 Elliptical Cavities h/D =0.47 Cavity Base ExperimentalSimulated Ground Plane SimulatedExperimental Cavity Side Simulated Experimental Cavity Base (modified scaling) Simulated

18 University of Western Ontario Department of Mechanical & Materials Engineering Advanced Fluid Mechanics Research Group Discussion and Questions are welcome An Experimental Investigation of Turbulent Boundary Layer Flow over Surface-Mounted Circular Cavities J. Dybenko and E. Savory, UWO 12:20-12:45 May 24, 2006 (Walker)


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