Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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- Consider a point in a structural member that is subjected to plane stress. Normal and shear stresses acting on horizontal and vertical planes at the point are shown. If 0 = 44 MPa in the direction shown, determine the principal stresses at the point. 85 MPa 56 MPa O 70.9 MPa and -97.0 MPa 82.8 MPa and -136.0 MPa 89.5 MPa and -64.2 MPa 75.1 MPa and -124.1 MPa 64.9 MPa and -105.9 MPaarrow_forward3. The shaft in the figure below consists of 75 mm diameter bronze segment that is rigidly joint to 50 diameter steel segment. The ends of the shaft are attached to rigid supports (fixed supports). Calculate the absolute maximum shear stress developed in each segment when the torque T = 5.1 kN-m is applied (a = 2 m and b = 1.5 m). Use G = 35 GPa for %3D %3D %3D bronze, and G = 75 GPa for steel. %3D 75 mm 50 mm A Bronze Steel C T a -arrow_forward1) A square cross-section cantilever beam is subjected to a force as shown below. What is the maximum force that can be applied to achieve a safety factor on yielding of 1.2 (use the maximum shear stress failure theory)? T = 8N-m L = 10m C=0.5m P=? Al 2024 Sy=455MPa Kic=26MPa (m)1/2arrow_forward
- For the beam shown below, b = 5 in and h = 12 in. If the beam is subjected to a transverse shear for of V = 8 kip, determine the largest shearing stress in the beam. Express your answer in psi to the nearest whole psiarrow_forwardA beam of rectangular cross-section 40 x 20 mm is loaded with tensile force 1000 N as shown in figure. A B BO Calculate the shear stress on oblique plane at 0 = 45° A 0.625 MPa C 0.31 MPa F D 1.25 MPaarrow_forwardFor the beam shown below, b = 6 in and h = 14 in. If the beam is subjected to a transverse shear for of V = 8 kip, determine the largest shearing stress in the beam. Express your answer in psi to the nearest whole psiarrow_forward
- A cube of side 100 mm is subjected to an axial compressive load of 200 kN. Its lateral strain is prevented by applying uniform pressure but only one fourth of lateral strain could be prevented, then which of the following statements is/are correct? Assume E = 200 MPa and μ = 0.3. A The decrease in length in direction of load after applying pressure is 9.358 x 10-3 mm. B The uniform pressure applied has a value of 8.57 N/mm². C The uniform pressure applied has a value of 2.14 N/mm². D The increase in length in lateral direction after applying pressure is 2.25 x 10-³ mm.arrow_forwardCalculate the design moment strength Mu for the following section. Take f'c = 40 MPa. Sketch the strain and stress distribution diagrams for each section and try to work out your solutions using equilibrium conditions. Yield stress for N bars is 500 MPa. 75 700 60 1500 T 4N28 450arrow_forward
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