Aspect ratio is defined as: The Wing Span divided by the average chord (b/cav) Ratio of the Chord at the tip to the chord at the root (Ct /Cr) Angle between the line of 25% chord points and the longitudinal axis Ratio of Lift to Drag Aspect ratio is defined as: The Wing Span divided by the average chord (b/cav) Ratio of the Chord at the tip to the chord at the root (Ct /Cr) Angle between the line of 25% chord points and the longitudinal axis Ratio of Lift to Drag The Wing Span divided by the average chord (b/cav) Ratio of the Chord at the tip to the chord at the root (Ct /Cr) Angle between the line of 25% chord points and the longitudinal axis Ratio of Lift to Drag
Explanation / Answer
The Wing Span divided by the average chord (b/cav)