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Determine the normal stress in rod AC of the wing. The following information is given: AAC = 200 mm2; a=2.5 m; b=2 m; w=3.5 k

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free body daigram W=3.5kN/m -- Filoso at Farcoso o By R AR & Farsine FAC 2.5m + t 2m - 2.5m FAL tano - 2.5 o tant (2) - 21.80please ask if any doubt

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