How to Calculate the Volume of an Aircraft Wing?

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To calculate the volume of an aircraft wing, one method involves multiplying the average area of the tip and root chords by the span. However, this approach may yield inaccurate results due to the wing's shape. A more precise technique is to calculate the area at multiple sections along the wing and apply numerical integration methods, such as Simpson's Rules. This allows for a more accurate representation of the wing's volume. Accurate volume calculation is essential for various aerodynamic analyses.
Ziv7
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How do u calculate the volume of an aircraft wing?


Would it work if I calculate the area of tip and root chord then times it by the span?

Thanks
 
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That's one way, but the answer might not be accurate depending on the shape of the wing. A better way would be to calculate the area of several different sections, and then use one of the rules for numerical integration (See Simpson's Rules).
 

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