Question: 4.4 Starting with ' Equation (4.35), derive L' Equation (4.36). 4.5 Consider a thin, symmetric airfoil at 1.5 angle of attack. From the results of
4.4 Starting with ' Equation (4.35), derive L' Equation (4.36). 4.5 Consider a thin, symmetric airfoil at 1.5 angle of attack. From the results of thin airfoil theory, calculate the lift coefficient and the moment coefficient about the leading edge
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