QuestionJune 5, 2025

How do we calculate the "Wing Area" of an airfoil? Divide the maximum chord width by the span Multiply the mean camber by the span Divide the span by the average chord width Divide the minimum chord width by the span Multiply the span by the average chord width

How do we calculate the "Wing Area" of an airfoil? Divide the maximum chord width by the span Multiply the mean camber by the span Divide the span by the average chord width Divide the minimum chord width by the span Multiply the span by the average chord width
How do we calculate the "Wing Area" of an airfoil?
Divide the maximum chord width by the span
Multiply the mean camber by the span
Divide the span by the average chord width
Divide the minimum chord width by the span
Multiply the span by the average chord width

Solution
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Answer

Multiply the span by the average chord width Explanation 1. Identify the correct formula The wing area of an airfoil is calculated by multiplying the span by the average chord width.

Explanation

1. Identify the correct formula<br /> The wing area of an airfoil is calculated by multiplying the span by the average chord width.
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