(40) the flexibility method down 1.5 inches and the support at D 4-Analyze the frame shown...
Analyze the Frames shown below. Draw the shear and moment
diagrams and sketch the approximate deflected shape
Settlement at A = 1” and at C = .5” E = 30000 kis, I = 240
in4
2k/ft 8 k B EI EI 36 k-ft С 12'1 EI A 12' 8'
draw the shear and bending moment diagrams also please
For the continuous beam shown, compute the support reactions using the method of consistent deformations by taking the reaction at support B as redundant. Also, draw the shear and bending moment diagrams. The beam is subjected to a 20 kips concentrated load at the middle of the left span plus a 1.5 inch settlement of support B. Use deflection formulas to determine deflections at B. Assume E-29000 ksi and I-750 in...
Problem 3 Analyze the frame structure subjected to the following support movements: a beam-end settlement at Node #4; . a column base rotation at (Node #1). All members have a constant bending stiffness El and are considered as axially rigid. a) Determine the degree of kinematic indeterminacy (DKI) and show the independent DOFs. b) Assemble the structure stiffness matrix Kg. c) Assemble the structure fixed-end force vector Po. Then solve for nodal displacement vector Us based on the equations of...
The queen-post trussed beam is used to support a uniform load of 4 k/ft. Determine the force developed in each of the five struts. Neglect the thickness of the beam and assume the truss members are pin connected to the beam. Also, neglect the effect of axial compression and shear in the beam. The cross-sectional area of each strut is 3 in2, and the moment of inertia for the beam is 600 in4. Also, E 29(103) ksi. Prob. 9-36 4...
Solve all problems using the finite element stiffness method. For the rigid frame shown in Figure P5-4, determine (1) the nodal displacements and rotation at node 4, (2) the reactions, and (3) the forces in each element. Then check equilibrium at node 4. Finally, draw the shear force and bending moment diagrams for each element. LetE 30 x 103 ksi, A = 8 in,2 , and 1-800 in.4 for all elements. 20 kip 25 ft 25 ft- 40 ft 20...
Solve all problems using the finite element stiffness method. For the rigid frame shown in Figure P5-4, determine (1) the nodal displacements and rotation at node 4, (2) the reactions, and (3) the forces in each element. Then check equilibrium at node 4 Finally, draw the shear force and bending moment diagrams for each element. Let E 30x 103 ksi, A 8 in2, and I 800 in.4 for all elements. 20 kip 25 ft 25 ft 40 ft Figure P5-4...
1. (60 points) Draw axial, shear, and bending moment diagrams for the frame shown below. Draw one set of P, V, and M diagrams for Column AB, one set for Beam BE, and one set for Column DF. There is a fixed support at A and applied forces and moments as shown below. 500 lb 500 lb 5 k-ft 5 k-ft D 5 k-ft B 10 10' 10' E 500 lb/ft 10' 10' 5k s tiskt 5 k-ft 1k 2....
15 marks Question 3 Consider the frame shown in Figure Q3 for which all elements have constant stiffness EL. Implement the flexibility method by removing the vertical support at A to create a statically determinate system. The Volume Integral Table is found on page 8 of this examination paper Find the reactions at A and D considering that node C is equidistant to nodes D (a) and B [12 marks] (b) Draw the bending moment diagram for the frame. 13...
3. (40 pts) Analyze the following statically determinate frame by hand and clearly draw the shear force, axial force, and bending moment diagrams indicating relevant (maximum and minimum) values for each of the following load cases: a) Uniform dead load (q) applied on the beam must add beam self-weight (concrete) to this value b) Uniform live load (qu) applied on the beam. c) Horizontal wind force (H H=12kip 12 x 20 gp-1.4 kip/ft -2.0 kip/ft 14 ft 12" x 12...
Problem 10.19 Consider the frame shown in (Figure 1). Assume the support at A is fixed and C is a pin. EI is constant. Part A Determine the internal end moment MBA acting on member AB of the frame at B measured clockwise. Express your answer using three significant figures. Enter positive value if the moment is clockwise and negative value if the moment is counterclockwise. MBA = 40.8 k ft Submit Previous Answers Correct Part B Determine the internal...