Question: Consider a thin, symmetric alifoll at ( 1 . 3 5 ^ { circ } ) angle of attack. From the results

Consider a thin, symmetric alifoll at \(1.35^{\circ}\) angle of attack. From the results of thin alffoll theory, calculate the lift coefficient and the moment coefficient about the leading edge. (Round the final answers to three decimal places.)
The lift coefficient is
The moment coefficlent about the leading edge is
Consider a thin, symmetric alifoll at \ ( 1 . 3 5

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