Calculate Moment About the Center of Gravity CG

 Method to Calculate the Moment about the Center of Gravity CG for a Given Wing Body Configuration

• Calculate Moment about the Center of Gravity (CG)

• Calculate Moment about Aerodynamic Center

• Calculate location of Aerodynamic Center and Value of Cmac

• Calculate Longitudinal Static Stability of Airplane

• Calculate Cmcg of Airplane

• Calculate Neutral Point of Airplane

• Calculate Static Margin of Airplane

• Calculate Elevator Deflection Angle to Trim the Airplane

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Moment about the Center of Gravity

In order to Calculate the moment about the center of gravity CG for a given wing body configuration we must enter the value of aerodynamic center which lies ahead of the center of gravity CG.

The value of the Moment Coefficient about the Aerodynamic center is also required for the calculation and Enter the lift Coefficient.

Doing the Calculation, the Value fo CM (cg) of Wing Body Configuration is Computed.

CM, cg (wb) = CM, ac(wb) + CL,(wb)[h-h,ac(wb)]

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