A simply supported beam AB is subjected to a triangle loading (see figure). The moment curvature...
A simply supported beam AB is subjected to a triangle loading (see figure). The moment curvature equation is shown (from the left). The (El=constant) 1. Determine the deflection at middle beam. 2. Determine the rotation at middle beam. 2 kN/m A B 4 m 8 d2v EI dx2 x3 12 *+z*
A simply supported beam AB is subjected to a triangle loading (see figure). The moment curvature equation is shown (from the left). The (El-constant) 1. Determine the deflection at middle beam. 2. Determine the rotation at middle beam. 2 kN/m A B 4.m x3 EI dx2 = - 2 COM MacBook Air 20 COD F4 FS F6 ►II # $ دیا 4 % 5 6 & 7 8 9
A simply supported beam AB is subjected to a triangle loading (see figure). The moment curvature equation is shown (from the left). The (El-constant) 1. Determine the deflection at middle beam. 2. Determine the rotation at middle beam. 2 kN/m B 4 m 8 EI 12 MacBook Air DOO 008 A tA % A - 5 & 7 6 I 0 * 8 9 R T
A cantilever beam AB is subjected to a triangle loading with concentrated moment (see figure). The moment curvature equation is shown (from the left). (El=constant) 1. Determine the deflection at point A. 2. Determine the rotation at point A. 3 kN/m 15 kN-m A B 6 m d2v ΕΙ 5x3 3 x2 – 15 2 dx2 6
Acantilever beam AB is subjected to a triangle loading with concentrated moment (see figure). The moment curvature equation is shown (from the left). (El=constant) 1. Determine the deflection at point A. 2. Determine the rotation at point A. 3 kN/m 15 kN-m B 6 m d2v EI dx- 5x3 3 --x2 - 15 6 2
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,...
QUESTION 1 [15] For the simply supported beam subjected to the loading shown in the figure, a) Derive equations for the shear force V and the bending moment M for any location in the beam. (Place the origin at point A.) b) Report the maximum positive bending moment, the maximum negative bending moment, and their respective locations. 36 KN 180 KN-m X B C D 4 m 5 m 3 m Figure 1
The simply supported bearm is made of A-36 steel and is subjected to the loading shown in (Figure 1. Suppose that P 18 kN. E 200 GPa and I - 0.1457(10 Part A Determine the deflection of the beam at its center C Express your answer to three signiticant tigures and include the appropriate units. Enter positive value If the deflection is upward and negative value If the deflection is downward. Ac= Value Units Figure 1 of 1 Submit Request...
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...
QUESTION 34 The simply supported beam shown in the figure below is subjected to a 3 kN concentrated force. The beam has modulus of elasticity of E-70 GPa and area moment of inertia equals to l-126x10-6 m4 Question 34- Question 38] 3 kN 5 According to successive integration method Ely(x) = x3 (x-2)3 6 12 4 () x2 8 (x+ 1)2 4 QUESTION 36 C2 = 0 QUESTION 36 C2 - 0 2 3 QUESTION 37 C1- 1.33 1.5 2.3...