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Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap

Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap

Ahmed Hassan

Details

OL Work ID
OL11624344W

Subjects

Trailing edge flapsComputational gridsAerodynamic characteristicsBlade-vortex interactionGrid generation (Mathematics)AirfoilsNoise reductionNavier-Stokes equation

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