Aspect ratio is defined as: The Wing Span divided by the average chord (b/ cav )
ID: 2277246 • Letter: A
Question
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 DragExplanation / Answer
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