Solution:- the figure(diagram) given in the question are as follows:
considering each span simply supported-
Calculating bending moment under load:-
bending moment at C(Mc)=16 kN-m
A1=(1/2)*10.285*7=35.9975
A1=35.9975
XL1=7+4/3
XL1=3.667 m
XR1=7+3/3
XR1=3.333 m
A2=(1/2)*12*6=36
A2=36
XL2=XR2=6/2=3 m
Apply three moment equation-
for A-B-C
MA(L1/I1)+MB(L1/I1+L2/I2)+Mc(L2/I2)+(6*A1*XL1)/(L1*I1)+(6*A2*XR2)/(L2*I2)=0 , [Eq-1]
where, MA=0
L1=7 m , L2=6 m
I1=1 , I2=2
A1=35.9975 , A2=36
values put in above equation-(1)
0+MB(7+6/2)+Mc(6/2)+(6*35.9975*3.667)/(7*1)+(6*36*3)/(6*2)=0
10*MB+3*MC+113.145+54=0
10*MB+3MC+167.145=0 , [Eq-2]
where, MC=16 kN-m
10*MB+3*(-16)+167.145=0
10*MB+119.145=0
MB=-119.145/10
MB=-11.9145 kN-m ,(negative sign represent only anticlockwise moment)
bending moment at support B(MB)=11.914 kN-m (anticlockwise)
bending moment at A(MA)=0
bending moment at C(Mc)=16 kN-m , (anticlockwise)
[Ans]
Q 4. A beam is shown in the figure given below where A is hinged, and...
Question 1: Consider the beam below. Please use the table below to determine the appropriate values for your question. The effects of self-weight are negligible compared to effects of the applied loading. Draw the bending moment diagram (BMD) and shear force diagram (SFD), clearly indicating the values of V & Mat A, B, C, & D Also show the location(s) and value(s) of maximum sagging and/or hogging moment. Include your working. L2 L3 Group 2A Li (mm) w (kN/m)P (kN)...
By stiffness method : determine the displacements at Joint B and at Joint C in the three-span beam shown in the figure below. The flexural rigidity of the beam is EI and is constant along the length of the beam. Note that L1 = L2 = L3 = L P1 = P2 = P3 = P M = PL wL = P Also, find the reactions at Joint A. い12 8 い12 8
Find all the reaction forces Ax, Ay,Dx,Dy Problem 1 The frame shown in the figure has two pin supports at points A and D. Two point loads P1 = P2 = 4 kN and a uniformly distributed load W = 10 kN/m are applied to the frame as shown. The horizontal reaction at support A is -1.037 kN. Note: A positive value here indicates a reaction force pointing to the right, and a negative value one pointing to the left....
Question 26: Draw M diagram for the beam and loading shown in figure 34, USE slope- deflection equations. El is constant. Given: L1= 5m L2= 1m L3= 5m F= 10 KN W= 10 KN/m M=17 KN.m W +11/2+11/2 2/2 315/2
L1(m)=1.5. L2(m)=1.5. w(kN/m)=3. P(kN)=10. M(kNm)= 8. B(mm)= 12. D(mm)=18 Q 4. Draw SFD and BMD for the beam given below and determine the absolute maximum bending stress in the beam if it has a rectangular cross-section of width (B) and depth (D). [7 marks) w kN/m PKN M kNm A B E 4 22 L1 L2 L2
Using the moment distribution method to solve the beam shown below. Take w = 15.8 kN/m and L 4.9 m ΒΣ 2EI EI 2L Part 3 Calculate the moment at B Мв kN m Part 4 Calculate the reaction force at C Cy kN
A continuous beam ABC shown in Figure 2 is fixed at A. Supports at B and C are rollers. A uniform distributed load 40kN/m is applied force acts downward on the span of BC as shown in Figure 2. The EI of the beam is over the span of AB and a 60kN constant (a) Determine the internal moments at A and B using the slope-deflection method [10 marks] (b) Draw the bending values of bending (c) Sketch the deformed...
Q5: Using force method, determine the reactions of the supports for the beam shown in Figure (5). Then draw shear and bending moment diagrams for the beam. EI is constant. Use conjugate beam method to determine deflections. I need it in 30min or 1 h 6 m 50 KN 200 kN.m 22 А В. С 9 m to 3m
Draw the Shear Force (V) and Bending Moment (MI) diagrams of statically indeterminate beam shown in figure using “Force Method”. The (roller) support at "B" settles 35 mm. The moment of inertia is given by (1) for regions "AB", "BC" and "CD"; however it is equal to (21) for the region “DE”. ("B" is the roller and “E" is the fixed type of support). [The flexural rigidity: EI=40000 kNm] 60 KN y 10 kN/m A - Tu (21) 1.5m 11...
For the beam given below, determine the resultant internal loading acting on the cross section at C. Use the following assumption: The beam is weightless. Support A is a roller, and support B is a pin. The cross section C is 1 m away from A. (Tips: Internal loading includes normal force, shear force, and moment). . 100 kN 50 kN/m ol B 2m 1m 2m