Question
The box beam shown represents a hypothetical wing-rib. For rib C, calculate: (a) the shear flow in the webs adjacent to the vertical stiffeners ef, dc, and ab. (b) Determine the axial forces at points c and d slightly to the left and slightly to the right of the vertical stiffener cd.
30 E 2000 lb 800 lb 30 Front Upper ib spar, flange 7000 Ib Stiffener 1000 Ib 1000 lb 3000 lb 15. c/ 15- a Rear spar web Lo
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3889 10 11 12 13 14 5 16 17 18 19 20 21 22 23 24 25 26 27 28tuo0b 29 30 31 TUESDAY DECEMBER k50 346-019 OOOtb lo0ol 10 coniid

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