Lift due to Wing in Longitudinal Stability Formulas

Lift due to Wing is the lift force acting on the wing (only) of an aircraft. And is denoted by L_w. Lift due to Wing is usually measured using the Newton for Force. Note that the value of Lift due to Wing is always negative.

Formulas to find Lift due to Wing in Longitudinal Stability

fxLift due to Wing onlyGo

Longitudinal Stability formulas that make use of Lift due to Wing

fxTotal Lift of Wing-Tail CombinationGo

fxLift due to Tail onlyGo

List of variables in Longitudinal Stability formulas

fx Lift Force Go

fx Lift due to Tail Go

FAQ

What is the Lift due to Wing?

Lift due to Wing is the lift force acting on the wing (only) of an aircraft. Lift due to Wing is usually measured using the Newton for Force. Note that the value of Lift due to Wing is always negative.

Can the Lift due to Wing be negative?

Yes, the Lift due to Wing, measured in Force can be negative.

What unit is used to measure Lift due to Wing?

Lift due to Wing is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Lift due to Wing can be measured.

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