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Bar DE is aluminum and has a cross sectional area of 5000 m{{m}^{^{2}}}mm, Bar BC is steel and has a cross sectional area of 1300 m{{m}^{^{2}}}mm, Quiz on Stress-Strain Diagrams, Material Properties, and Shear Stress and Strain, Modulus of Elasticity: E = 50 GPa Proportional Limit: {{\sigma }_{Proportional Limit }}=0.075\,GPa\,\,σ, Modulus of Elasticity: E = 150 GPa Proportional Limit: {{\sigma }_{Proportional Limit }}=0.225\,GPa\,\,σ, Poisson’s Ratio: \nuν = 0.25 Young’s Modulus: E = 120 GPa, Poisson’s Ratio: \nuν = 0.6 Young’s Modulus: E = 200 GPa, The shear strain at point A is 1500 µ rad, The shear strain at point A is 95500 µ rad, The normal stress on plane AA is 50 MPa (T) and the magnitude of the shear stress on plane AA is 90 MPa, The normal stress on plane AA is 67.5 MPa (T) and the magnitude of the shear stress on plane AA is 72.7 MPa. Get Financial Aid for “Machine Learning” Course. Show a Mohr’s Circle plot depicting the principal stresses and the maximum in-plane shear stress for the stress condition acting at a point in an engineering structural member shown below. We first review the basic concepts of equilibrium and stresses and strains in prismatic bars under axial loading. Mechanics of Materials I: Fundamentals of Stress & Strain and Axial Loading course is offered by “Coursera”. The students enrolling in these courses can also earn a certificate for free of cost. Your email address will not be published. {{\varepsilon }_{x}}=\,-500\,\mu \,\frac{mm}{mm}ε x=−500μmmmm{{\varepsilon}_{y}}=\,1250\,\mu \,\frac{mm}{mm}ε y =1250μ mmmm {{\gamma }_{xy}}=\,1900\,\mu \,radγ xy N.B. The Science of Well-Being | Coursera | All 10 Week 100% Correct Quiz & Assignment Answers Free. Mindshift: Break Through Obstacles to Learning- Coursera Courses Quiz & Assignment Answers Free. Find the axial force in member JH. 2. and has a normal stress of 200 MPa in compression. 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Competitive Strategy Coursera Quiz Answers | 100 % Correct Answers Of Week (1-6) 15. Find the Factor of Safety with respect to yield and the Factor of Safety with respect to fracture. Show a Mohr’s Circle plot depicting the principal strains and the maximum in-plane shear strain for the strain condition below acting at a point in an engineering structural member. 3. Heat C. Mechanical D. Electrical Kinetic energy is the energy Take free online classes from 80+ top universities and organizations. A thin rectangular plate section of an airplane is uniformly deformed as shown below. We believe in connecting people to a great education so that anyone around the world can learn without limits. Week 2: Quiz 2 – Social Media Marketing Specialization Coursera Quiz Answers Summer 2018 This quiz is closed-book closed-notes, one 3" x 5"card allowed. Avoid extra spaces and punctuation. 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For an engineering structural member under loading, the strain components at a point are found to be{{\varepsilon}_{x}}=\,-500\,\mu\,\frac{mm}{mm}ε x =−500μ mmmm {{\varepsilon }_{y}}=\,1250\,\mu \,\frac{mm}{mm}ε y =1250μmmmm{\gamma }_{xy}}=\,1900\,\mu \,radγ xy =1900μradFind the strain components {{\varepsilon }_{n}}ε n and {{\gamma}_{nt}}γ nt Welcome! topics One of the world’s most widely known online learning platform, Coursera, is now offering more than 100 courses for free to everyone around the world till the end of december, 2020. This course explores the analysis and design of beam bending problems. 2004 quiz files. This module reviews the principles of the mechanics of deformable bodies. The yield stress of the steel is 250 MPa. 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For the engineering structure below you may assume the weight of the members to be negligible when compared to the loads they are supporting. for the n-t axes oriented as shown below: {{\varepsilon }_{n}}=\,415\,\mu \,\frac{mm}{mm}ε n =415μ mmmm and {{\gamma }_{nt}}=\,2560\,\mu \,radγ nt =2560μrad, {{\varepsilon }_{n}}=\,-709\,\mu \,\frac{mm}{mm}ε n =−709μ mmmm and {{\gamma }_{nt}}=\,-2560\,\mu \,radγ nt =−2560μrad, {{\varepsilon }_{a}}=\,750\,\mu \,\frac{mm}{mm}ε a=750μ mmmm {{\varepsilon }_{b}}=\,1250\,\mu \,\frac{mm}{mm}ε b =1250μ mmmm, {{\varepsilon }_{c}}=\,-50\,\mu \,\frac{mm}{mm}ε c =−50μ mmmm Find the strain components {{\varepsilon }_{x}},\,{{\varepsilon}_{y}},\,{{\gamma }_{xy}}ε x ,ε y ,γ xy at the point, 3.

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