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Engineering, 19.02.2021 03:50 SkirrtCrackers

2. Calculate the static pressure (normalized by the freestream pressure) acting on each edge ofthe diamond airfoil.3. Calculate theCdandClcoefficients for the diamond airfoil.4. Repeat the previous drawing/calculations for the truncated diamond airfoil (i. e., the wedge)5. By what percentage does the lift-to-drag ratio improve when the rear portion of diamondairfoil is retained

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