Structural Analysis, 5th Edition
Structural Analysis, 5th Edition
5th Edition
ISBN: 9788131520444
Author: Aslam Kassimali
Publisher: Cengage Learning
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Chapter 4, Problem 22P
To determine

Find the forces in the members of the truss by the method of joints.

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Answer to Problem 22P

The forces in the members of the truss are

FAE=81.87k(C)_, FAC=102.18k(T)_, FEG=89.49k(C)_, FEC=56.57k(T)_, FCG=73.89k(T)_, FCD=60k(T)_, FBF=70.47k(C)_, FBD=39.27k(T)_, FFG=62.83k(C)_, FFD=56.57k(T)_, and FDG=10.94k(T)_.

Explanation of Solution

Given information:

Apply the sign conventions for calculating reactions, forces and moments using the three equations of equilibrium as shown below.

  • For summation of forces along x-direction is equal to zero (Fx=0), consider the forces acting towards right side as positive (+) and the forces acting towards left side as negative ().
  • For summation of forces along y-direction is equal to zero (Fy=0), consider the upward force as positive (+) and the downward force as negative ().
  • For summation of moment about a point is equal to zero (Matapoint=0), consider the clockwise moment as negative and the counter clockwise moment as positive.

Method of joints:

The negative value of force in any member indicates compression (C) and the positive value of force in any member indicates Tension (T).

Calculation:

Consider the forces in the member AE, EG, AC, CG, BF, FG, BD, DG, CD, CE, and DF are FAE,FEG,FAC,FCG,FBF,FFG,FBD,FDG, FCD,FCE,FDF.

Show the free body diagram of the truss as shown in Figure 1.

Structural Analysis, 5th Edition, Chapter 4, Problem 22P , additional homework tip  1

Refer Figure 1.

Consider the horizontal and vertical reactions at A are Ax and Ay.

Consider the vertical reaction at B is By.

Calculate the value of the angle θ as follows:

tanθ=2525θ=tan1(1)θ=45°

Calculate the value of the angle α as follows:

tanβ=1010β=tan1(1)β=45°

Calculate the value of the angle α as follows:

tanα=3515α=tan1(3515)α=66.80°

Calculate the value of the angle γ as follows:

tanγ=1535γ=tan1(1535)γ=23.198°

Take the sum of the forces in the vertical direction as zero.

Fy=0Ay+By=40        (1)

Take the sum of the forces in the horizontal direction as zero.

Fx=0Ax+10+20+10=0Ax=40k

Take the sum of the moments at A is zero.

MA=0(By×100)(10×35)(20×25)(20×50)(20×75)(10×35)=0By×100=3700By=37k

Substitute 37k for By in Equation (1).

Ay+37=40Ay=3k

Show the joint A as shown in Figure 2.

Structural Analysis, 5th Edition, Chapter 4, Problem 22P , additional homework tip  2

Refer Figure 2.

Find the forces in the member AC and AE as follows:

For Equilibrium of forces,

Fy=0Ay+FAEsinα+FACsinθ=03+FAEsin(66.80°)+FACsin(45°)=03+0.9191FAE+0.7071FAC=00.9191FAE+0.7071FAC=3        (2)

Fx=0Ax+FAEcosα+FACcosθ=040+FAEcos(66.80°)+FACcos(45°)=040+0.3939FAE+0.7071FAC=00.3939FAE+0.7071FAC=40        (3)

Subtract Equation (2) from Equation (3).

0.5252FAE=43FAE=430.5252FAE=81.87k(C)

Substitute 81.87k for FAE in Equation (3).

0.3939×(81.87)+0.7071FAC=400.7071FAC=40+0.3939×(81.87)FAC=40+0.3939×(81.87)0.7071FAC=102.18k(T)

Show the joint E as shown in Figure 3.

Structural Analysis, 5th Edition, Chapter 4, Problem 22P , additional homework tip  3

Refer Figure 3.

Find the forces in the member EC and EG as follows:

For Equilibrium of forces,

Fy=0FEAsinαFECsinβ+FEGsinγ=0(81.87)sin66.80°FECsin45°+FEGsin23.198°=075.2490.7071FEC+0.3939FEG=00.3939FEG0.7071FEC=75.249        (4)

Fx=010FAEcosα+FECcosβ+FEGcosγ=010(81.87)cos66.80°+FECcos45°+FEGcos23.198°=010+32.252+0.7071FEC+0.9191FEG=00.9191FEG+0.7071FEC=42.252        (5)

Solve Equation (4) and (5).

FEG=89.49kFEG=89.49k(C)

FEC=56.57kFEC=56.57k(T)

Show the joint C as shown in Figure 4.

Structural Analysis, 5th Edition, Chapter 4, Problem 22P , additional homework tip  4

Refer Figure 4.

Find the forces in the member CG and CD as follows:

For Equilibrium of forces,

For Equilibrium of forces,

Fy=0FECsinβ+FCGsinθFCAsinθ20=0FECsin45°+FCGsin45°FCAsin45°20=056.57×0.7071+0.7071FCG0.7071FCA20=0

20+0.7071FCG0.7071FCA=0FCG=20+0.7071FCA0.7071FCG=20+0.7071×(102.18)0.7071FCG=73.89k(T)        (6)

Fx=0FECcosβ+FCGcosθFCAcosθ=0FECcos45°+FCGcos45°FCAcos45°+FCD=00.7071FEC+0.7071FCG0.7071FCA+FCD=0

0.7071×(56.57)+0.7071×(73.89)102.18+FCD=060+FCD=0FCD=60k(T)        (7)

Show the joint B as shown in Figure 5.

Structural Analysis, 5th Edition, Chapter 4, Problem 22P , additional homework tip  5

Refer Figure 5.

Find the forces in the member BF and BD as follows:

For Equilibrium of forces,

Fx=0FBFcosαFBDcosθ=0FBFcos66.80°FBDcos45°=00.394FBF+0.707FBD=0        (8)

Fy=0FBFsinα+FBDsinθ+By=0FBFsin66.80°+FBDsin45°+37=00.919FBF+0.707FBD=37        (9)

Solve Equation (8) and (9).

FBF=70.47k(C)FBD=39.27k(T)

Joint F

Show the joint F as shown in Figure 6.

Structural Analysis, 5th Edition, Chapter 4, Problem 22P , additional homework tip  6

Refer Figure 6.

Find the forces in the member EC and EG as follows:

For Equilibrium of forces,

Fx=0FFGcosγFFDcosβ+10+FFBcosα=0FFGcos23.198°FFDcos45°+10+FFBcos66.80°=00.919FFG0.707FFD+10+0.3939(70.47)=00.919FFG0.707FFD=17.758        (10)

Fy=0FFGsinγFFDsinβFFBsinα=0FFGsin23.198°FFDsin45°FFBsin66.80°=00.3939FFG0.707FFD(70.47)×0.919=00.3939FFG0.707FFD=64.761        (11)

Solve Equation (10) and (11).

FFG=62.83k(C)FFD=56.57k(T)

Joint D:

Show the joint D as shown in Figure 7.

Structural Analysis, 5th Edition, Chapter 4, Problem 22P , additional homework tip  7

Refer Figure 7.

Find the forces in the member DG as follows:

For Equilibrium of forces,

Fx=0FDCFDGcosθ+FDFcosβ+FDBcosθ=0FDCFDGcos45°+FDFcos45°+FDBcos45°=060FDGcos45°+56.57cos45°+39.24cos45°=0FDG=7.737cos45°FDG=10.94k(T)

Thus, the forces in the members of the truss are

FAE=81.87k(C)_, FAC=102.18k(T)_, FEG=89.49k(C)_, FEC=56.57k(T)_, FCG=73.89k(T)_, FCD=60k(T)_, FBF=70.47k(C)_, FBD=39.27k(T)_, FFG=62.83k(C)_, FFD=56.57k(T)_, and FDG=10.94k(T)_.

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Students have asked these similar questions
5-1. Determine the force in each member of the truss, and state if the members are in tension or compression.
I have the correct answer provided, just lookng for a more detailed breadown of how the answer was obtained thanks.
Q1. Statically indeterminate beam analysis. a) Calculate the BMs (bending moments) at all the joints of the beam shown in Fig.1 using the moment distribution method. The beam is subjected to an UDL of w kN/m. L1= 0.4L. Assume the support at C is pinned, and A and B are roller supports. E = 200 GPa, I=250x106 mm². Use the values of w = 50 kN/m and L = 6 b) Draw the shear force and bending diagrams for the entire beam. c) Calculate the BMs at all the joints of the same beam shown in Fig.1 using the slope deflection method. d) Compare the values of BMs obtained using the two methods a) and c) and comment. w kN/m £1m Lm m Fig 1. Beam for Q1
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