Question: Wing span (s) Wing root chord length ( c ) Wing tip chord length ( c ) Planform area (S) Chord length along span

Wing span (s) Wing root chord length ( c ) Wing tip

Wing span (s) Wing root chord length ( c ) Wing tip chord length ( c ) Planform area (S) Chord length along span (c(y)) Torsional rigidity of the wing (GJ) 1.1m 0.374m 0.2m 0.3157 m cy=-0.1581 y+0.374 GJ (y)=1500 (1.5-0.5 y)

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