Current Attempt in Progress The simply supported beam consists of a W24 x 94 structural steel wide-flange shape [E = 29,000 ksi; I = 2,700 in.4]. For the loading shown, determine the beam deflection at point C. Assume P = 39 kips, w = 2.7 kips/ft, LAB = 13 ft, LBc= LcD= 7 ft. B |C D LAB LBC LCD Answer: Vc= in.

The simply supported beam consists of a W14 × 34 structural steel wide-flange shape [E = 29,000 ksi; I = 340 in.4].  For the loading shown, use discontinuity functions to compute (a) the slope of the beam at E and (b) the deflection of the beam at C.  Assume w0 = 7 kips/ft, wCD = 5.5 kips/ft, LAB = 7.0 ft, LBC = 7.0 ft, LCD = 9.5 ft, LDE = 4 ft.

The simply supported beam consists of a W14 × 34 structural steel wide-flange shape [E = 29,000 ksi; I = 340 in.4].  For the loading shown, use discontinuity functions to compute (a) the slope of the beam at E and (b) the deflection of the beam at C.  Assume w0 = 11 kips/ft, wCD = 5.0 kips/ft, LAB = 7.5 ft, LBC = 7.5 ft, LCD = 11.0 ft, LDE = 4 ft.

The simply supported beam consists of a W530 × 66 structural steel wide-flange shape [E = 200 GPa; I = 351 × 106 mm4]. Assume w = 45 kN/m, L1 = 2.6 m, and L2 = 2.6 m. For the loading shown, determine:(a) the beam deflection at point B.(b) the beam deflection at point D. Part 6 Determine the component of the beam deflection at point D produced by the component of the rotation angle of the beam at point C due to only the portion of the uniformly distributed load w between the supports at point A and point C.Answer: vD1 =          mm. Part 7 Determine the component of the beam rotation angle at point C due to the moment produced at point C by the portion of the uniformly distributed load w between point C and point D.Answer: θC2=          rad.   Part 8 Determine the component of the beam deflection at point D due to the moment produced at point C by the portion of the uniformly distributed load w between point C and point D.Answer: vD2 =…