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Aircraft Mechanics
Aspect Ratio of a Wing in Introduction and Governing Equations Formulas
The Aspect Ratio of a wing is defined as the ratio of its span to its mean chord. And is denoted by AR.
Introduction and Governing Equations formulas that make use of Aspect Ratio of a Wing
f
x
Drag Coefficient for given parasite drag coefficient
Go
f
x
Drag Coefficient for given zero-lift drag coefficient
Go
f
x
Coefficient of Drag due to lift
Go
FAQ
What is the Aspect Ratio of a Wing?
The Aspect Ratio of a wing is defined as the ratio of its span to its mean chord.
Can the Aspect Ratio of a Wing be negative?
{YesorNo}, the Aspect Ratio of a Wing, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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