As shown in figure, a simple supported beam carries two symmetrically placed concentrated loads. Compute the maximum deflection. A 3 m 100 N 100 N 3 m 3 m B

The beam shown in the figure is subjected to a moment of M = 50 kN.m. Determine the bending stress at point A and B.

Prob 5. Calculate the maximum deflection dmax and the angle of deflection on the supports of a uniformly loaded simple beam loaded as shown. The maximum bending stress is o=60 MPa. The cross section of the beam is square with a length of 8 cm on each side. The beam is made of aluminum having modulus of elasticity E = 70 GPa. q = 2.0 kN/m L= 2.0 m

Hw1: For the simply supported beam shown in Figure, determine the maximum deflection due to the applied load. The flexural rigidity of the beam is El= 7x106 kip.in². V₁ = 20 kips a = 12 ft 1 = 18 ft Answer: ymax = -0.129 ft downward W = 60 kips b = 6 ft 2 V₂ = 40 kips