I am planning to measure the wing area of a Spitfire aircraft. I am going to use double integral formula, but firstly I need to derive the continuous function for the region of interest. Also,(adsbygoogle = window.adsbygoogle || []).push({});

How to do that? I searched the entire internet and only found out the wing span of that aircraft, cant find the width or the fuselage (part of the wing inside the aircraft, which doesnt count)

Thank you

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# How to work out the area of an elliptical wing?

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