Determine the centroid coordinates (x̄ , ȳ) for the beam section shown in Figure Q6. Give your answer relative to the origin (O) in millimetres (mm) and to two decimal places. 2. Calculate the second moment of area about its centroidal x-axis for the L-shaped section shown in Figure Q6. Assume the beam section is the solid and homogeneous. Give your answer in mm4 to two decimal places. 3. Calculate the maximum tensile stress [σtensile_max] and the maximum compressive stress [σcompressive_max] for the beam in Figure Q6. *Assume that the weight of the beam is zero and that the beam section is solid and uniform along its entire length. Give your answer in N/mm2 to 2 decimal places.
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Determine the centroid coordinates (x̄ , ȳ) for the beam section shown in Figure Q6. Give your answer relative to the origin (O) in millimetres (mm) and to two decimal places.
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2. Calculate the second moment of area about its centroidal x-axis for the L-shaped section shown in Figure Q6. Assume the beam section is the solid and homogeneous. Give your answer in mm4 to two decimal places.
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3. Calculate the maximum tensile stress [σtensile_max] and the maximum compressive stress [σcompressive_max] for the beam in Figure Q6. *Assume that the weight of the beam is zero and that the beam section is solid and uniform along its entire length. Give your answer in N/mm2 to 2 decimal places.
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