SAN4701 JAN/FEB 2015 QUESTION 1 The truss shown in Figure 1 is hinged at C, B and D It is acted upon at node A by a ver...
SAN4701 OCT/NOV 2014 QUESTION 1 Determine the member forces in the symmetrical truss shown in Figure 1 The panels are assumed to be square with all the members having a constant EA of 35 x 103 kN [30 MARKS] 4M 10 KN
SAN4701 OCT/NOV 2014 QUESTION 1 Determine the member forces in the symmetrical truss shown in Figure 1 The panels are assumed to be square with all the members having a constant EA of 35 x 103 kN [30...
SAN4701 OCT/NOV 2013 QUESTION 3 (30 marks) Determine the member forces and vertical deflection at node C in the truss shown in Figure 3. Material property is constant throughout the members i.e EA -50 x 10° KN. 2 8 kN 3 m 4 4 m
SAN4701 OCT/NOV 2013 QUESTION 3 (30 marks) Determine the member forces and vertical deflection at node C in the truss shown in Figure 3. Material property is constant throughout the members i.e EA -50 x...
QUESTION 3 The truss shown in the Figure 3 is having hinged supports at A and B, assuming that the EA is constant for all the members. Use a flexibility method to determine the forces in each member and reactions at the supports. 80 kN 5 m 5 m 5 m 5 m Figure 3 130 marks) Total Marks [100
QUESTION 3 The truss shown in the Figure 3 is having hinged supports at A and B, assuming that the...
SAN4701 OCT/NOV 2016 QUESTION 3 The frame shown in the Figure 3 is having a fixed support at A and a hinged at support D Determine the reactions at the supports and moments at the joints using flexıbility method El is constant 20 kN/m 3 m 40 kN 3 m Figure 3 [30 marks] TOTAL MARKS [100] UNISA 2016
SAN4701 OCT/NOV 2016 QUESTION 3 The frame shown in the Figure 3 is having a fixed support at A and a...
Analyse the beam shown in Figure 4 using the stiffiness method. Node D is fixed and node 2 and 3 are rollers. A uniform distributed load of 1 kN/m is acting on member 1 . And a load of 10 kN is acting at the middle of member2. EI is constant for all members a) Identify the force vector of the structure; [4 marks] b) Identify the displacement vector of the structure; [2 marks] c) Determine the stiffness matrices of...
SAN4701 OCT/NOV 2017 QUESTION 1 The beam shown in Figure 1 is fixed at support A and support C, support B is a roller support. Use the stiffness matrix method to determine the. Member stiffness matrix 11 1.2 Structure and load matrix (10) 13 Displacement matrix Reactions at the support 14 15. Moments at the fixed supports El is constant along the length of the beam 18 kN 10 kN 20 m 10 m 1 15 m15 m Figure 1...
SAN4701 JAN/FE8 2017 QUESTION 1 1 is having a hinge support at 1 and a roller support at 2. (E - 200 GPa) for all the members and the members 1, d 3 have their cross sectional areas as 4000 mm2, 4000 mm2 and 6000 mm2 The truss shown in Figure Assuming that E is constant respectively, use the matrix stiffness method to determine the following Number of degrees of freedom. a. (15) b. Structure stiffness matrıx. (10) c Member...
Analyse the ten members truss structure shown in Figure 02 using Compatibility Method and calculate the axial force acting on member EC Take the Young's Modulus and the cross-sectional area of each member to be constant. 2(a) (15 marks 5 m 20 35 kN Figure Q2: Ten members truss b) Find the force in member BC 3 marks) Find the force in member BF 2 marks)
2. For the pin-jointed truss shown in Figure Q2.1 applied at node 4. The Young's modulus E(GPa) is the same for the three truss vertical downward force P(kN) is a members. The cross sectional area of each of the truss members is indicated below and expressed in terms of a constant A. By using the stiffness method: (a) Compute the reduced stiffness matrix Kg [5 marks [10 marks (b) Calculate the global displacements of node 4 in terms of P,...
13. Based on the stiffness method, determine the stiffness matrix K for the truss shown in figure. Use the stiffness matrix to calculate the unknown displacement (D1 and D2) at the node where the load 5 kN and 10 kN are applied, and then determine the reactions at the pinned supports (Q3, Q4, Q5 and 26). Note that the degrees of freedom (DOFs) of the truss are indicated in the figure. Take EA as constant. The supports are pinned. 4....