(a)
Find the vertical displacement of joint C.
(a)

Answer to Problem 4P
The vertical deflection at joint C (δCy) is −0.364 in.↓_.
Explanation of Solution
Given information:
Area of members AB, BC, and CD are 1 in.2 and area of members AE, ED, BE, and CE are 0.25 in.2.
The value of E is 10,000 ksi.
Procedure to find the deflection of truss by virtual work method is shown below.
For Real system: If the deflection of truss is determined by the external loads, then apply method of joints or method of sections to find the real axial forces (F) in all the members of the truss.
For virtual system: Remove all given real loads, apply a unit load at the joint where is deflection is required and also in the direction of desired deflection. Use method of joints or method of sections to find the virtual axial forces (Fv) in all the member of the truss.
Finally use the desired deflection equation.
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 (∑Mat a point=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).
Condition for zero force members:
If only two non-collinear members are connected to a joint that has no external loads or reactions applied to it, then the force in both the members is zero.
If three members, two of which are collinear are connected to a joint that has no external loads or reactions applied to it, then the force in non-collinear member is zero.
Calculation:
Find the bar forces FP produced by the P-system as follows:
Let Ax and Ay be the horizontal and vertical reactions at the hinged support A.
Let Dy be the vertical reaction at the roller support D.
Find the reactions at the supports using equilibrium equations:
Summation of moments about A is equal to 0.
∑MA=0Dy(22)−15(11)+10(8)=0Dy=3.86 kips↑
Summation of forces along y-direction is equal to 0.
+↑∑Fy=0Dy+Ay−15=03.86+Ay−15=0Ay=11.14 kips↑
Summation of forces along x-direction is equal to 0.
+→∑Fx=0Ax−10=0Ax=10 kips→
Find the member forces using method of joints:
Apply equilibrium equation to the joint A:
+↑∑Fy=011.14+FABsin53.13°=0FAB=−13.92 kips
+→∑Fx=010+FAE+FABcos53.13°=010+FAE+(−13.92)cos53.13°=0FAE=−1.648 kips
Apply equilibrium equation to the joint D:
+↑∑Fy=03.86+FCDsin53.13°=0FCD=−4.83 kips
+→∑Fx=0−FED−FCDcos53.13°=0−FED−(−4.83)cos53.13°=0FED=2.898 kips
Apply equilibrium equation to the joint B:
+↑∑Fy=0−FABsin53.13°−FBEsin57.99°=0−(−13.92)sin53.13°−FBEsin57.99°=0FBE=13.133 kips
+→∑Fx=0−FABcos53.13°+FBEcos57.99°−10+FBC=0−(−13.92)cos53.13°+(13.133)cos57.99°−10+FBC=0FBC=−5.312 kips
Apply equilibrium equation to the joint C:
+↑∑Fy=0−FCDsin53.13°−FCEsin57.99°=0−(−4.830)sin53.13°−FCEsin57.99°=0FCE=4.556 kips
Sketch the bar forces produced by the P-system as shown in Figure 1.
Consider a dummy load of 1 kN directed vertically at joint C with the bar forces FQ.
Find the reactions at the supports using equilibrium equations:
Summation of moments about A is equal to 0.
∑MA=0−Dy(22)+1(16)=0Dy=0.727 kips↓
Summation of forces along y-direction is equal to 0.
+↑∑Fy=0−Dy+Ay+1=0−0.727+Ay+1=0Ay=0.273 kips↓
Summation of forces along x-direction is equal to 0.
+→∑Fx=0Ax=0
Find the member forces using method of joints:
Apply equilibrium equation to the joint A:
+↑∑Fy=0−0.273+FABsin53.13°=0FAB=0.341 kips
+→∑Fx=0FAE+FABcos53.13°=0FAE+(0.341)cos53.13°=0FAE=−0.205 kips
Apply equilibrium equation to the joint D:
+↑∑Fy=00.727+FCDsin53.13°=0FCD=0.909 kips
+→∑Fx=0−FED−FCDcos53.13°=0−FED−(0.909)cos53.13°=0FED=−0.545 kips
Apply equilibrium equation to the joint B:
+↑∑Fy=0−FABsin53.13°−FBEsin57.99°=0−(0.341)sin53.13°−FBEsin57.99°=0FBE=−0.322 kips
+→∑Fx=0−FABcos53.13°+FBEcos57.99°+FBC=0−(0.341)cos53.13°+(−0.322)cos57.99°+FBC=0FBC=0.375 kips
Apply equilibrium equation to the joint C:
+↑∑Fy=0−FCDsin53.13°−FCEsin57.99°+1=0−(0.909)sin53.13°−FCEsin57.99°+1=0FCE=0.322 kips
Sketch the bar forces FQ produced by the vertical dummy load Cy as shown in Figure 2.
Refer Table 1 for vertical displacement of joint C.
(b)
Find the horizontal displacement of joint C.
(b)

Answer to Problem 4P
The horizontal deflection at joint C (δCx) is −0.269 in.←_.
Explanation of Solution
Given information:
Area of members AB, BC, and CD are 1 in.2 and area of members AE, ED, BE, and CE are 0.25 in.2.
Calculation:
Consider a dummy load of 1 kN directed horizontally at joint C with the bar forces FQ.
Find the reactions at the supports using equilibrium equations:
Summation of moments about A is equal to 0.
∑MA=0Dy(22)−1(8)=0Dy=0.363 kips↑
Summation of forces along y-direction is equal to 0.
+↑∑Fy=0Dy+Ay=00.363+Ay=0Ay=0.363 kips↓
Summation of forces along x-direction is equal to 0.
+→∑Fx=0Ax=1 kip←
Find the member forces using method of joints:
Apply equilibrium equation to the joint A:
+↑∑Fy=0−0.363+FABsin53.13°=0FAB=0.455 kips
+→∑Fx=0FAE+FABcos53.13°=0FAE+(0.455)cos53.13°−1=0FAE=0.727 kips
Apply equilibrium equation to the joint D:
+↑∑Fy=00.363+FCDsin53.13°=0FCD=−0.455 kips
+→∑Fx=0−FED−FCDcos53.13°=0−FED−(−0.455)cos53.13°=0FED=0.273 kips
Apply equilibrium equation to the joint B:
+↑∑Fy=0−FABsin53.13°−FBEsin57.99°=0−(0.455)sin53.13°−FBEsin57.99°=0FBE=−0.429 kips
+→∑Fx=0−FABcos53.13°+FBEcos57.99°+FBC=0−(0.455)cos53.13°+(−0.429)cos57.99°+FBC=0FBC=0.5 kips
Apply equilibrium equation to the joint C:
+↑∑Fy=0−FCDsin53.13°−FCEsin57.99°=0−(−0.455)sin53.13°−FCEsin57.99°=0FCE=0.492 kips
Sketch the bar forces FQ produced by the horizontal dummy load Cx as shown in Figure 3.
Refer Table 1 for horizontal displacement of joint C.
(c)
Find the horizontal displacement of joint D.
(c)

Answer to Problem 4P
The horizontal deflection at joint D (δDx) is 0.066 in.→_.
Explanation of Solution
Given information:
Area of members AB, BC, and CD are 1 in.2 and area of members AE, ED, BE, and CE are 0.25 in.2.
Calculation:
Consider a dummy load of 1 kN directed horizontally at joint D with the bar forces FQ.
Find the reactions at the supports using equilibrium equations:
Summation of moments about A is equal to 0.
∑MA=0Dy=0
Summation of forces along y-direction is equal to 0.
+↑∑Fy=0Ay=0
Summation of forces along x-direction is equal to 0.
+→∑Fx=0Ax=1 kip←
Find the member forces using method of joints:
Apply equilibrium equation to the joint A:
+↑∑Fy=0−1+FAB=0FAB=1 kips
Apply equilibrium equation to the joint D:
+↑∑Fy=01−FED=0FED=1 kips
The force in the member AB, BE, EC, BC, and CD are zero as it satisfies zero force member condition.
Sketch the bar forces FQ produced by the horizontal dummy load Dx as shown in Figure 4.
Find the vertical deflection at joint C (δCy) using the relation:
(1 kips)(δCy)=∑FPFQLAE
Find the horizontal deflection at joint C (δCy) using the relation:
(1 kips)(δCx)=∑FPFQLAE
Find the product of FQFPLAE for each member as shown in Table 1.
Bar |
A (in.2) |
L (ft) | FP(kips) | FQ(kips) | FQFPLAE(in.) | |||||
Cx | Cy | Dx | Cx | Cy | Dx | |||||
AB | 1 | 10 | −13.920 | 0.455 | 0.341 | 0 | −0.076 | −0.057 | 0 | |
BC | 1 | 10 | −5.312 | 0.500 | 0.375 | 0 | −0.032 | −0.024 | 0 | |
CD | 1 | 10 | −4.830 | −0.455 | 0.909 | 0 | 0.026 | −0.053 | 0 | |
DE | 0.25 | 11 | 2.898 | 0.273 | −0.545 | 1 | 0.042 | −0.083 | 0.153 | |
EA | 0.25 | 11 | −1.648 | 0.727 | −0.205 | 1 | −0.063 | 0.018 | −0.087 | |
EB | 0.25 | 9 | 13.133 | −0.429 | −0.322 | 0 | −0.255 | −0.191 | 0 | |
EC | 0.25 | 9 | 4.556 | 0.429 | 0.322 | 0 | 0.089 | 0.066 | 0 | |
δP=∑FQFPLAE | −0.269 | −0.364 | 0.066 |
Refer Table 1.
The vertical deflection at joint C (δCy) is −0.364 in.↓_.
The horizontal deflection at joint C (δCx) is −0.269 in.←_.
The horizontal deflection at joint D (δDx) is 0.066 in.→_.
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Chapter 8 Solutions
Fundamentals Of Structural Analysis:
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