Thank you for answering this question. Please you specify each step as soon as possible.Good Luck! Thank You.For a 60° angle lamina that subjected loads shown below,15 MPaT3.5 MPa1.4 MPaOx = -3.5 MPa, oy = 15 MPa, Txy = -1.4 MPaCalculate the stresses in L-T directions (ơ1, ơr, TLt)Determine whether the lamina will fail under these applied loads by using Tsai-Hill failure criteria.Determine whether the lamina will fail under these applied loads by using maximum stress failurecriteria.Mechanical properties:EL = 14 GPa; ET=3.5 GPA; GLT = 4.2 GPa; vt = 0.40Strength (In case of tension): OLU = 250 MPa, ơTu =10 MPaStrength (In case of compression): OLU = 200 MPa, ơTu = 0.5 MPaShear strength: TLTU = 8 MPaOT+OLu+<1Tsai-Hill criterion:OLu-OLu

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Engineering

Mechanical Engineering

subjected loads s.

Mechanics of Materials (MindTap Course List)

9th Edition

ISBN:9781337093347

Author:Barry J. Goodno, James M. Gere

Publisher:Barry J. Goodno, James M. Gere

Chapter7: Analysis Of Stress And Strain

Section: Chapter Questions

Problem 7.7.15P: A brass plate with a modulus of elastici ty E = 16 X 106 psi and Poisson’s ratio a = 0.34 is loaded...

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