Aerospace Engineering > GATE 2017 > Thin-walled Structures
The idealized cross section of a thin-walled wing box structure shown in the figure is subjected to an anticlockwise torque of 10 kNm. The corresponding shear-flow distribution under this loading condition is shown in the figure. The area of each cell is A1=300x103mm2 and A2=250x103mm2.
The ratio of the unknowns x/y is given by _______ (in three decimal places).
Correct : 0.640 to 0.650
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