Right is a cross-section of a fuselage; the inner structure is supported/attached to the outer structure by two beams. Determine the shear flow distribution for a torque of T=65,000 Nm for this multi-cell section. Cell Area [mm] I 110,000 II 220,000 III 540,000 Wall Length [mm] Thickness G [N/mm] [mm] 12upper 1200 1.5 20,000 12lower 2200 1.8 20,000 14, 23 150 1.1 30,000 34upper 750 1.2 25,000 34lower 800 1.2 25,000 I 2 II 1 3 4 III