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Flow Prediction for Variable Angle of Attack Analyzing Lift And Drag Coefficient of An Aerofoil Subjected To Different Turbulence Effects

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Figure

Fig 2: Far field Boundaries
Fig 4: Variation of Drag in INVISCID flow.
Fig 8: Pressure contours For 80 INVISCID flow
Fig 12: Pressure contours For 160 INVISCID flow
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