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Aircraft Mechanics
Lift Curve Slope in Static Stability and Control Formulas
The Lift Curve Slope refers to a characteristic parameter in aerodynamics that quantifies the change in lift coefficient with respect to the change in angle of attack of an airfoil or wing. And is denoted by Cl
α
.
Static Stability and Control formulas that make use of Lift Curve Slope
f
x
Lift given Roll Rate
Go
f
x
Lift Coefficient with respect to Roll Rate
Go
FAQ
What is the Lift Curve Slope?
The Lift Curve Slope refers to a characteristic parameter in aerodynamics that quantifies the change in lift coefficient with respect to the change in angle of attack of an airfoil or wing.
Can the Lift Curve Slope be negative?
{YesorNo}, the Lift Curve Slope, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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