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m04_ps02_spring04 - at the tip The beam has a rectangular...

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Unified Engineering Spring 2004 Problem M4 The spar in a wing is modeled as a 10 m long beam. The combination of lift and self-weight is modeled as resulting in a load distribution varying linearly from 5kN/m at the root to zero
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Unformatted text preview: at the tip. The beam has a rectangular cross section, height, h, of 100 mm and breadth, b, of 50 mm. Calculate the maximum bending stress in the beam, stating its location(s) and calculate the deflection of the tip of the beam...
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