Question: A rectangular wing with a constant symmetric aerofoil section along its entire span is to be designed to be elliptically loaded at cruise conditions
A rectangular wing with a constant symmetric aerofoil section along its entire span is to be designed to be elliptically loaded at cruise conditions using twist. The angle of attack at the centre of the wing is 8 degrees. What does the angle of attack need to be half way along the semi-span?
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