Problem 2. A dogbone tension specimen of a material is shown in figure. Longitudinal position and...
Strength of material
2) An aluminum specimen with a defeet as shown having a thickness of 2 mm width 22 mm, the defeet has a hole of 4.S mm radius, the crack length is 12.5 mm from tip to tip the length of the specimen was 65 mm , this specimen is subjected to a tensile fore up to 6200 N, it fractured at s4s0 Find the ultimate stress. 10 marks
2) An aluminum specimen with a defeet as shown...
Question 3 For the simply supported steel beam with cross section and loading shown (see Figure 3a), knowing that uniformly distributed load w=60 kN/m, Young modulus E = 200 GPa, and yield stress Cyield=200 MPa (in both tension and compression). ул 15 mm w=60 kN/m ... 1 B A 15 mm + 300 mm IC - i 2.5m 1 1 15 mm 7.5m 1 150 mm Figure 3a (a) Check if: the beam is safe with respect to yielding (using...
40kN Uniform Load W kN/m X Span L L/2 Figure 1 SPAN L 6 W 11Kn/m Beam is 200 UB 18.2 Use the diagram above and the W and L values assigned to you to: a) Use your shear force diagram to calculate the Maximum longitudinal Shear Stress and where it occ Ccurs. b) Calculate the longitudinal Shear Stress at d/4 from the neutral axis. Check Figures 283 below this table BENDING MOMENT DIAGLAM Kp/m f:40 zm 7.5 KN-M 90...