Given: Composite beam is made of material 'A’ on top and 'B’ on bottom with dimensions shown. trop M = 6.5 kN-m Etop = 200 GPa Ebottom = 100 GPa b = 175 mm tpottom B- M ttop = 50 mm tbottom = 200 mm b

Find the maximum flexural stress in the bottom material.

Given: Composite beam is made of material 'A’ on top and 'B’ on<br>bottom with dimensions shown.<br>trop<br>M = 6.5 kN-m<br>Etop = 200 GPa<br>Ebottom = 100 GPa<br>b = 175 mm<br>tpottom<br>B-<br>M<br>ttop = 50 mm<br>tbottom = 200 mm<br>b<br>

Extracted text: Given: Composite beam is made of material 'A’ on top and 'B’ on bottom with dimensions shown. trop M = 6.5 kN-m Etop = 200 GPa Ebottom = 100 GPa b = 175 mm tpottom B- M ttop = 50 mm tbottom = 200 mm b

Jun 10, 2022

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Given: Composite beam is made of material 'A’ on top and 'B’ on bottom with dimensions shown. trop M = 6.5 kN-m Etop = 200 GPa Ebottom = 100 GPa b = 175 mm tpottom B- M ttop = 50 mm tbottom = 200 mm b

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