Pitching Moment due to Tail in Longitudinal Stability Formulas

Pitching Moment due to Tail is the pitching moment of the tail about the aircraft’s center of gravity. And is denoted by M_t. Pitching Moment due to Tail is usually measured using the Newton Meter for Moment of Force. Note that the value of Pitching Moment due to Tail is always negative.

Formulas to find Pitching Moment due to Tail in Longitudinal Stability

fxTail Pitching Moment for given Lift CoefficientGo

fxPitching Moment due to TailGo

fxTail Pitching Moment for given Moment CoefficientGo

Longitudinal Stability formulas that make use of Pitching Moment due to Tail

fxTail Lift for given Tail Pitching MomentGo

fxMean Aerodynamic Chord for given Tail Pitching Moment CoefficientGo

fxTail Pitching Moment CoefficientGo

fxTail Lift Coefficient for given Pitching MomentGo

List of variables in Longitudinal Stability formulas

fx Horizontal Tail Moment Arm Go

fx Tail Lift Coefficient Go

fx Freestream Density Go

fx Velocity Tail Go

fx Horizontal Tail Area Go

fx Lift due to Tail Go

fx Tail Pitching Moment Coefficient Go

fx Flight Velocity Go

fx Reference Area Go

fx Mean Aerodynamic Chord Go

FAQ

What is the Pitching Moment due to Tail?

Pitching Moment due to Tail is the pitching moment of the tail about the aircraft’s center of gravity. Pitching Moment due to Tail is usually measured using the Newton Meter for Moment of Force. Note that the value of Pitching Moment due to Tail is always negative.

Can the Pitching Moment due to Tail be negative?

Yes, the Pitching Moment due to Tail, measured in Moment of Force can be negative.

What unit is used to measure Pitching Moment due to Tail?

Pitching Moment due to Tail is usually measured using the Newton Meter[N*m] for Moment of Force. Kilonewton Meter[N*m], Millinewton Meter[N*m], Micronewton Meter[N*m] are the few other units in which Pitching Moment due to Tail can be measured.

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