Example: Given the aircraft multi-cellular structure below, determine the shear flow and angle of twist per unit length in each cell. ( G=25 times 10^{5} mathrm{~N} / mathrm{cm}^{2} ) and thickness of all walls are ( mathrm{t}=0.1 mathrm{~cm} ). The applied torque is ( 10,000 mathrm{~N}^{*} mathrm{~cm} ). [ T= sum 2 mathrm{Aq} ]

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Example: Given the aircraft multi-cellular structure below, determine the shear flow and angle of twist per unit length in each cell.  ( G=25  times 10^{5}  mathrm{~N} /  mathrm{cm}^{2}  ) and thickness of all walls are  (  mathrm{t}=0.1  mathrm{~cm}  ). The applied torque is  ( 10,000  mathrm{~N}^{*}  mathrm{~cm}  ).  [ T= sum 2  mathrm{Aq}  ]

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