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Aircraft Mechanics
Aspect Ratio of a Wing in Level Flight Formulas
The Aspect Ratio of a Wing is defined as the ratio of its span to its mean chord. And is denoted by AR.
Level Flight formulas that make use of Aspect Ratio of a Wing
f
x
Zero-Lift Drag Coefficient for given Lift Coefficient
Go
f
x
Lift Coefficient given Minimum required Thrust
Go
f
x
Zero-lift drag coefficient at minimum required thrust
Go
f
x
Minimum Thrust required for given Lift Coefficient
Go
f
x
Minimum Thrust required for given weight
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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