Problem 1 . (30%) The bar in Fig I. has a constant width of 35 mm...
4kN 150 mm 2kN Problem 1, subjected to two concentrated forces and has a as shown in the figures The cantilever beam, (fixed at A)s 0 mm30 mm -30 mm (a) Determine the maximum shear stress on the section (b) Determine the maximum bending stress in compression and in tension (c) If the allowable bending stress (for tension and compression) is ơao.-6 MPa, calculate the new minimum required section modulus. 4kN 150 mm 2kN Problem 1, subjected to two concentrated...
(A) 8 mm 100 mm Problem 1 (20 pts): Stress Concentrations Consider the flat bar with shoulder joints shown in Fig. A which is subjected to a tensile force P = 58 kN. The bar is made of Aluminum 6061 having maximum tensile strength Omax = 290 MPa. NOTE: plots of stress concentration factors for different types of loading can be found on page 6. (a) Determine the radius r [mm] for the fillets. (b) An identical flat bar shown...
(A) Smin 100 mm Problem 1 (20 pts): Stress Concentrations Consider the flat bar with shoulder joints shown in Fig. A which is subjected to a tensile force P = 58 kN. The bar is made of Aluminum 6061 having maximum tensile strength Omax = 290 MPa. NOTE: plots of stress concentration factors for different types of loading can be found on page 6 (a) Determine the radius r [mm] for the fillets. (b) An identical flat bar shown in...
A bar of 15mm x 15mm square cross-section is machined so as to reduce the thickness in a central region to 5mm, as shown in Figure 5. The bar is now subjected to a force F=2kN whose line of action passes through the centroid of the original square section. Sketch the distribution of stress in the reduced section and find the maximum tensile stress. By what factor does this exceed the average normal stress in the original section? 6. A...
A column with a wide-flange section has a flange width b = 400 mm , height h = 400 mm , web thickness tw = 13 mm , and flange thickness tf = 21 mm (Figure 1). Calculate the stresses at a point 65 mm above the neutral axis if the section supports a tensile normal force N = 3 kN at the centroid, shear force V = 7.4 kN , and bending moment M = 4 kN⋅m as shown...
4kN 150 mm 2kN Problem 1, subjected to two concentrated forces and has a as shown in the figures The cantilever beam, (fixed at A)s 0 mm30 mm -30 mm (a) Determine the maximum shear stress on the section (b) Determine the maximum bending stress in compression and in tension (c) If the allowable bending stress (for tension and compression) is ơao.-6 MPa, calculate the new minimum required section modulus.
(A) הודות ל 100 mm Consider the flat bar with shoulder joints shown in Fig. A which is subjected to a tensile force P = 58 kN. The bar is made of Aluminum 6061 having maximum tensile strength omax 290 MPa. NOTE: plots of stress concentration factors for different types of loading can be found on page 6. (a) Determine the radius r [mm] for the fillets. (b) An identical flat bar shown in Fig. B replaces the tensile load...
Problem 4 Two blocks of rubber each having a height h=300 mm, width w = 400 mm, and thickness a = 50 mm are used to make a shear spring as shown. The rubber has a shear modulus G = 2.5 MPa. A load P = 30 kN is applied. a) Determine the average shear stress in the rubber pads. b) Determine the average shear strain in the rubber pads. c) What is the relative displacement 8?
Sm 100 mm Consider the flat bar with shoulder joints shown in Fig. A which is subjected to a tensile force P-58 kN. The bar is made of Aluminum 6061 having maximum tensile strength Omar = 290 MPa. NOTE: plots of stress concentration factors for different types of loading can be found on page 6 (a) Determine the radiusr [mm] for the fillets. (b) An identical flat bar shown in Fig. B replaces the tensile load with a bending moment...
The cross section of the cantilever beam loaded as shown in Fig. 8-20 is rectangular, 50 × 75 mm. The bar, 1 m long, is aluminum for which E = 65 GPa. Determine the permissible maximum intensity of loading if the maximum deflection is not to exceed 5 mm and the maximum stress is not to exceed 50 MPa. Ans. w0 = 14.1 kN/m and 17.1 kN/m. Select 14.1 kN/m. oment 3 Fig. 8-20 oment 3 Fig. 8-20