Question: A thin cambered airfoil is approximated by three straight line segments as shown in the below figure. Calculate zero-lift angle of attack, coefficient of

A thin cambered airfoil is approximated by three straight line segments as shown in the below figure.

A thin cambered airfoil is approximated by three straight line segments as shown in the below figure. Calculate zero-lift angle of attack, coefficient of lift and moment coefficient about leading edge for an angle of attack of 3 degrees. (15 Marks) Y b 0 1 T 14 1 314 1 X

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SOLUTION To calculate the zerolift angle of attack coefficient of lift and moment coefficient about the leading edge for a thin cambered airfoil we need to use the following equations Zerolift angle o... View full answer

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