Question: Pitching moment co-efficient for an airfoil is given by ___

Options

A : lift*area

B : drag*area

C : section pitching moment/dynamic pitching moment

D : lift/dynamic moment

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Airfoil Selection-1 more questions

An airfoil is subjected to the flow with temperature of....

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Find location of aerodynamic centre from leading edge if, chord....

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The cross-sectional shape of wing is called ___

The parameter marked by '?' in the diagram is ___^

We are using the airfoil in the aircraft as ___

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Which of these is not part of an airfoil?

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