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Aerodynamics
Lift Curve Slope in Flow over Airfoils and Wings Formulas
The Lift Curve Slope is a measure of how rapidly the wing generates lift with a change in the angle of attack. And is denoted by a
C,l
. Lift Curve Slope is usually measured using the 1 per Radian for Reciprocal Angle. Note that the value of Lift Curve Slope is always negative.
Formulas to find Lift Curve Slope in Flow over Airfoils and Wings
f
x
Lift Curve Slope for Finite Wing
Go
f
x
Lift Curve Slope for Elliptic Finite Wing
Go
Flow over Airfoils and Wings formulas that make use of Lift Curve Slope
f
x
2D Lift Curve Slope of Airfoil given Lift Slope of Finite Wing
Go
f
x
2D Lift Curve Slope of Airfoil given Lift Slope of Elliptic Finite Wing
Go
f
x
Aspect Ratio of Wing given Lift Curve Slope of Elliptic Finite Wing
Go
f
x
Aspect Ratio of Wing given Lift Curve Slope of Finite Wing
Go
List of variables in Flow over Airfoils and Wings formulas
f
x
2D Lift Curve Slope
Go
f
x
Induced Lift Slope Factor
Go
f
x
Wing Aspect Ratio
Go
FAQ
What is the Lift Curve Slope?
The Lift Curve Slope is a measure of how rapidly the wing generates lift with a change in the angle of attack. Lift Curve Slope is usually measured using the 1 per Radian for Reciprocal Angle. Note that the value of Lift Curve Slope is always negative.
Can the Lift Curve Slope be negative?
Yes, the Lift Curve Slope, measured in Reciprocal Angle can be negative.
What unit is used to measure Lift Curve Slope?
Lift Curve Slope is usually measured using the 1 per Radian[rad⁻¹] for Reciprocal Angle. 1 per Degree[rad⁻¹], 1 per Minute[rad⁻¹], 1 per Quadrant[rad⁻¹] are the few other units in which Lift Curve Slope can be measured.
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