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3: Induced flow created on wing with and without winglets

3: Induced flow created on wing with and without winglets

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Thesis
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A numerical study was undertaken to study the effect of vertical fluid injection on the performance of a 3D wing at a velocity of 20 m/s and angle of attack of 6, 8, and 10 degree. A baseline configuration along with injection at three different velocities were studied where a slot is used at the tip of the wing to inject the fluid. A literature su...