Question
The lamina thickness of a composite [0/90/] plate is 10 mm. Given that the Young's modulus E for the laminas with O ^ 0 and
The lamina thickness of a composite [0/90/] plate is 10 mm. Given that the Young\\\'s modulus E for the laminas with O ^ 0 and 90° fiber direction are 45 GPa and 12 GPa, respectively. Find the bending stress o on the bottom and top surface of the plate when the bending moment M = 500 N.m is applied. Also, calculate the bending stiffness of the plate knowing that the width of the plate is 60 mm.
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Heat Transfer
Authors: Jack Holman
10th edition
73529362, 978-0073529363
