Agter finding unknown reactions we can write moment equation in integral form
then we can draw moment curve by assuming symmetry from both sides
apply boundary condition and then for strain energy integrate to find total strain energy (upto 0 to 0.5L then multiply by 2
i have shown calculations in my solution
Thanks
Q2. A simply supported beam AB (Figure 2) supports a uniformly distributed load of q =...
The simply supported beam of length L is subjected to uniformly distributed load of w and a vertical point load P at its middle, as shown in Figure Q3. Both young's modulus and second moment of area of this structure are given as E and I. Please provide your answers in terms of letters w, P,L,1, E. Self-weight of the beam is neglected. P W L/2 L/2 Figure Q3 (a) Determine the reactions, bending moment equation along the beam and...
4. For a simply supported beam AB with concentrated load at C, determine step-by-step (a) the graph for bending moment, (b) the elastic curve y(x) for 0<x< Land (b) the deflection at point C. The length of the beam L-a+b.
Q2 The simply supported beam of length is subjected to a vertical point load at its middle, as shown in Figure Q2. Both young's modulus and second moment of area of this structure are given as and. Please provide your answers in terms of letters. Self-weight of the beam is neglected. Figure Q2 (a) Determine the reactions, bending moment equation along the beam and draw the corresponding bending moment diagram [10] (b) Determine both the slope and deflection at the...
Problem 2 Consider a simply supported symmetric I beam ABCD carrying a uniformly distributed load w and a concentrated load F as shown in Figure 2. Young's modulus of the beam is 200 GPa F- 8 kNN 8cm 3cm 3cm w- 6 kN/m 6cm 2cm Figure 2 1) Replace the support C with the reaction force Rc, and using static equilibrium find the reactions at point A and B in terms of Ro 2) Using the boundary conditions, calculate the...
Q2 The simply supported beam of length L is subjected to a vertical point load P at its middle, as shown in Figure Q2. Both young's modulus and second moment of area of this structure are given as E and I. Please provide your answers in terms of letters P,L,1, E. Self-weight of the beam is neglected. P L/2 L/2 Figure Q2 (a) Determine the reactions, bending moment equation along the beam and draw the corresponding bending moment diagram. [10]...
Q2 The simply supported beam of length L is subjected to a vertical point load P at its middle, as shown in Figure Q2. Both young's modulus and second moment of area of this structure are given as E and I. Please provide your answers in terms of letters P,L,1,E. Self-weight of the beam is neglected P L/2 L/2 Figure Q2 (a) Determine the reactions, bending moment equation along the beam and draw the corresponding bending moment diagram. [10] (b)...
Problem 2 Consider a simply supported symmetric I beam ABCD carrying a uniformly distributed load w and a concentrated load F as shown in Figure 2. Young's modulus of the beam is 200 GPa. F 8 kN 8cm 3cm 3cm 7 m 5 m 3 m 2cm W= 6 kN/m 6cm A D B 2cm 7TITT TITIT Figure 2 1) Replace the support C with the reaction force Rc, and using static equilibrium find the reactions at point A and...
16.6a) A simply supported beam is to span 15 ft. It will support a uniformly distributed load of 2 kips/ft over the full span and a concentrated load of 60 kips at mid-span. What is the required plastic section modulus Zx? (Include self-weight) 16.6b) A simply supported beam is to span 15 ft. It will support a uniformly distributed load of 2 kips/ft over the full span and a concentrated load of 60 kips at mid-span. Deflection is not to...
The simply supported beam AB in Figure 1 is subjected to a load variation given by w(x) = -kr". ܨܝ܂ Figure 1 (a) Determine the equation of the elastic curve in terms of El, x and L. (El is constant) (15 Points) (b) The beam has a length L of 1 m. Determine, in terms of k: (1) The reaction at the roller support. (3 Points) (ii) The bending moment at the section 0.2 m from end A, (that is,...
(2) A simply supported beam of flexural rigidity El carries a constant uniformly distributed load of intensity p per unit length as shown Figure 2 below. Assume the deflection shape to be a polynomial in x, and is given by v (x) = a., + as+ a2 x, where ao, a.呙are constants to be determined. (a) State the boundary conditions for the deflection equation. Using the boundary conditions stated in (a) and the Rayleigh-Ritz method, determine (b) the constants a,...