Re-derive the coefficient of pitching moment equation for the aircraft in the previous problem.Note: Use the...

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Mechanical Engineering

Re-derive the coefficient of pitching moment equation for theaircraft in the previous problem.Note: Use the corresponding freebody diagram and build-up method for the derivation.

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The Moment about the CG centre of gravity of the aircraft ina broad sense is created by 4 factors1Lift Drag and Moment about the aerodynamic centre ofthe wing2 Lift of the tail3 The Thrust of engine4 Aerodynamic forces and moments of other partsAssuming    See Answer
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