Wing Zero Lift Angle in Longitudinal Stability Formulas

The wing zero lift angle, relative to the fuselage reference line, refers to the angle formed between the chord line of the wing and the reference line of the fuselage. And is denoted by α_0,w. Wing Zero Lift Angle is usually measured using the Radian for Angle. Note that the value of Wing Zero Lift Angle is always positive.

Longitudinal Stability formulas that make use of Wing Zero Lift Angle

fxPitching Moment Coefficient for Fuselage ContributionGo

fxCoefficient of Pitching Moment Respect to Fuselage ContributionGo

FAQ

What is the Wing Zero Lift Angle?

The wing zero lift angle, relative to the fuselage reference line, refers to the angle formed between the chord line of the wing and the reference line of the fuselage. Wing Zero Lift Angle is usually measured using the Radian for Angle. Note that the value of Wing Zero Lift Angle is always positive.

Can the Wing Zero Lift Angle be negative?

No, the Wing Zero Lift Angle, measured in Angle cannot be negative.

What unit is used to measure Wing Zero Lift Angle?

Wing Zero Lift Angle is usually measured using the Radian[rad] for Angle. Degree[rad], Minute[rad], Second[rad] are the few other units in which Wing Zero Lift Angle can be measured.

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