Question Cagtegory: Aerodynamics
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With the angle of attacck alpha of 5° and h/c = 0.06
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The lift coefficient on a spinning circular cylinder in a freestream with a velocity of 24 and at an altitude …
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An oblique shock wave with a wave angle \(\beta\) is generated from a wedge angle of \(\theta\).What is the ratio …
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Write a MATLAB code for a source flow at the origin.
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Write a matlab code for vortex panel method.
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