Assume that M0 = 5.90 kN-m and L = 5.50 m. Determine the reaction at support B. Assume that EI is constant for the beam.

Assume that M0 = 4.90 kN-m and L = 3.70 m. Determine the reaction at support B. Assume that EI is constant for the beam.

Determine the beam deflection at point H. Assume that EI = 3.99 × 1010 kN-mm2 is constant.

A structural steel wide-flange shape [E = 232 GPa; I = 201 × 106 mm4] is loaded and supported as shown. The beam is supported at B by a 20-mm-diameter solid aluminum [E = 88 GPa] rod. After a concentrated load of 40 kN is applied to the tip of the cantilever, determine the force produced in the aluminum rod.

A structural steel wide-flange shape [E = 242 GPa; I = 201 × 106 mm4] is loaded and supported as shown. The beam is supported at B by a 20-mm-diameter solid aluminum [E = 90 GPa] rod. After a concentrated load of 40 kN is applied to the tip of the cantilever, determine the force produced in the aluminum rod.

Determine the beam deflection at point H. Assume that EI = 3.72 × 1010 kN-mm2 is constant.

For the beam loaded as shown, use the method of superposition to determine the beam deflection at point H. Assume that EI = 1.92 × 107 kips-in.2 is constant.

A structural steel wide-flange shape [E = 222 GPa; I = 201 × 106 mm4] is loaded and supported as shown. The beam is supported at B by a 20-mm-diameter solid aluminum [E = 80 GPa] rod. After a concentrated load of 40 kN is applied to the tip of the cantilever, determine the force produced in the aluminum rod.

Determine the beam deflection at point H. Assume that EI = 2.57 × 1010 kN-mm2 is constant.

Assume that w0 = 150 N/m and L = 4 m. Determine the bending-moment equation M(x) for this beam and loading.