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Aerodynamics
Wing Aspect Ratio in Flow over Airfoils and Wings Formulas
Wing Aspect Ratio is defined as the ratio of the square of wingspan to the wing area or wingspan over wing chord for a rectangular planform. And is denoted by AR.
Formulas to find Wing Aspect Ratio in Flow over Airfoils and Wings
f
x
Aspect Ratio given Span Efficiency Factor
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
Flow over Airfoils and Wings formulas that make use of Wing Aspect Ratio
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
Oswald Efficiency Factor
Go
f
x
Lift Curve Slope for Finite Wing
Go
f
x
Lift Curve Slope for Elliptic Finite Wing
Go
List of variables in Flow over Airfoils and Wings formulas
f
x
Lift Coefficient
Go
f
x
Span Efficiency Factor
Go
f
x
Induced Drag Coefficient
Go
f
x
2D Lift Curve Slope
Go
f
x
Lift Curve Slope
Go
f
x
Induced Lift Slope Factor
Go
FAQ
What is the Wing Aspect Ratio?
Wing Aspect Ratio is defined as the ratio of the square of wingspan to the wing area or wingspan over wing chord for a rectangular planform.
Can the Wing Aspect Ratio be negative?
{YesorNo}, the Wing Aspect Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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