MECH2040 2017 SPRING TERM FINAL EXAM Part I: Basic Concepts (40 points) 1. For problems (a), (b) shown in Fig.1, write down the boundary conditions at point O and A for problem (a) and (b), and the continuity conditions at point B for problem (b). (10 points) Fig.1 2. (1) For problems (a) and (b) in Fig.2, determine the minimum critical force Pcr of in-plane buckling and draw a schematic buckling curve at the minimum critical force Pcr. The in-plane bending stiffness is EI and the effective length of column for various end conditions is shown in Fig.3. (10 points) Fig.2 Fig.3 Effective length of column for various end conditions (2) For the three kinds of possible buckling modes under critical compressive forces (PA, PB, PC) shown in Fig.4, which of the following is correct? β PA> PB> PC, β‘ PB> PC> PA, β’ PC> PB> PA, β£ PA> PC> PB, (Tip: The Buckling force for the buckling curve y(x) = A sin πππ₯ πΏ is Pππ = π2 π2 πΈπΌ πΏ2 ) (5 points) Fig.4 3. (1) A cubic element is in plane stress state and the stress components on surface A is marked on its Mohr’s Circle as shown in Fig.5, β Please draw the stress state of this element; β‘ The maximum tensile stress of this element = and is oriented at degree with the positive x axis. (5 points) Fig.5 (2) A cubic element is in plane stress state and the stress components on surface A is marked on the Mohr’s Circle as shown in Fig.6, β Please draw the stress state of this element; β‘ The maximum shear stress of this element = and is oriented at degree with the positive x axis. (5 points) Fig.6 (3) A cubic element is in plane stress state and the Mohr’s Circle of this element shrinks to a point (σ = −2π0 ) as shown in Fig.7, β Please draw the stress state of this element; β‘ The maximum shear stress = . (5 points) Fig.7 Part II: Calculation (60 points) 1. For the beam and loading shown below, (a) find the state of stress at point A in the Cartesian coordinate system indicated in the figure. (b) use Mohr’s circle to determine (i) the principal stress and principal plane; (ii) the normal and shearing stresses acting on a plane oriented at 450 indicated in the figure. The parameters are: πΏ = 1π, β = 20ππ, π = 10ππ, π = 1ππ β π, π = 150ππ. Figure 1 2. A mass π at β = 1π falls onto a beam at point A. Given the length of the beam πΏ = 1π, π = 2ππ, πΈπΌ = 100ππ β π2 , π₯ = 0.3π, and neglect the gravity, calculate (a) the maximum deflection of point A; (b) the maximum deflection of the entire beam. Figure 2 3. The overhanging beam ABCD supports a concentrated force P and a uniform load with intensity q as shown below. For what ratio P/(qa) will the deflection at point D be zero? Use the method of superposition to solve this problem and you are allowed to use any formula given. Figure 3