Discussion
Wing fuel volume scales roughly with thickness ratio and chord squared. Reducing thickness from \( 12 \) to \( 10 \) per cent at constant chord changes the volume by
Answer: A
The volume falls in proportion to thickness, so \( 10/12 = 0.833 \), a reduction of about seventeen per cent. On a design already tight for tank space this can be the constraint that stops the wing being thinned further.
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