QUESTION 33 The simply supported beam shown in the figure (18) below is subjected to a...
QUESTION 33 A simply supported steel beam with two eccentric loads as shown in the figure (17) below. The second moment of area of the beam section about the neutral axis is ( 1-0.201 x 10 mm). And the modulus of elasticity (E 207 GPa) Al dimensions in mm), Answer (Question 33-Question 361 3.5 kN 2.1 kN E 207 x 10" Pa 300. Figure (17) The support reaction at point A in the y direction (RAy):(CLO6) (a Point) 2.71 KN...
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...
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
Question 2 Simply supported beam ABC is subject to a point load and the patch loads as indicated in Figure Q2. Assume the beam has a uniform cross-section size. The Modulus of Elasticity E = 210x106 kN/m2, second moment of area l=5x105 m. Determine the deflection of beam ABC at the middle point using MacCaulay's Method. Total (15) marks. -30 KN -6 kN/m -3 kN/m B 3 m 4 m * Figure Q2: Simply supported beam ABC
QUESTION 34 For a simply supported beam with a single load at the midpoint, the predicted maximum deflection is given by Дмах PL3 48 EI PL :-.. Af Tel + L where P is the load, L is the length. E is the modulus of elasticity, and I is the moment of inertia. Referring to this diagram and equation, answer True or False: All else being equal, increasing modulus of elasticity will decrease the deflection True False
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P= 10 KN W = 10 kN/m 200 mm 5 m 5 m...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P = 10 kN W = 10 kN/m 200 mm 5 m 5...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P = 10 kN w = 10 kN/m 200 mm 5 m 5...
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...
Figure 1 shows a beam is supported by a pin at A and a roller at
C. The beam is subjected to point
loads 30 kN and 60 kN and a uniformly distributed load of 24 kN/m.
Modulus of elasticity, E and
moment of inertia, I for all members are 205 kN/mm2 and 195 x 106
mm4, respectively. By using
Virtual Work method,
(a) determine the slope at B. (1.801 mrad)
(b) determine the deflection at B and D. (2.4...