Q3. (30 pts) Simply supported beam under a uniformly distributed load with given

Question

Q3. (30 pts) Simply supported beam under a uniformly distributed load with given dimensions k- 1:200 mm Figure 3. Simply Supported Beam Under Uniformly Distributed Load Follow Example 6.1 in the textbook for given material in Q1: [0/90/0] symmetric laminate 3a. (10 pts) Calculate the maximum deformation max 3b. (20 pts) Calculate maximum tensile stress at the bottom of the bottom layer (Layer 3) Hint: You wil need transformed reduced stiffness matrix for the third layer [Qlk-3 It is already calculated in your tool. Note: Unit of the maximum moment found in 2b is [Nm]. You need Mz in [Nm/m]. Therefore, M,,max = Mmax/b

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Since this questn states you have follow the example 6.1 , which you have not been uploaded.

Neither you provide the data i.e the value of H, E(young modulus) for the Soln

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