FUND. OF STRUCTURAL ANALYSIS-W/ACCESS
FUND. OF STRUCTURAL ANALYSIS-W/ACCESS
17th Edition
ISBN: 9781260207286
Author: Leet
Publisher: MCG
Question
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Chapter 8, Problem 4P

(a)

To determine

Find the vertical displacement of joint C.

(a)

Expert Solution
Check Mark

Answer to Problem 4P

The vertical deflection at joint C (δCy) is 0.364in._.

Explanation of Solution

Given information:

Area of members AB, BC, and CD are 1in.2 and area of members AE, ED, BE, and CE are 0.25in.2.

The value of E is 10,000ksi.

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 (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).

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=3.86kips

Summation of forces along y-direction is equal to 0.

+Fy=0Dy+Ay15=03.86+Ay15=0Ay=11.14kips

Summation of forces along x-direction is equal to 0.

+Fx=0Ax10=0Ax=10kips

Find the member forces using method of joints:

Apply equilibrium equation to the joint A:

+Fy=011.14+FABsin53.13°=0FAB=13.92kips

+Fx=010+FAE+FABcos53.13°=010+FAE+(13.92)cos53.13°=0FAE=1.648kips

Apply equilibrium equation to the joint D:

+Fy=03.86+FCDsin53.13°=0FCD=4.83kips

+Fx=0FEDFCDcos53.13°=0FED(4.83)cos53.13°=0FED=2.898kips

Apply equilibrium equation to the joint B:

+Fy=0FABsin53.13°FBEsin57.99°=0(13.92)sin53.13°FBEsin57.99°=0FBE=13.133kips

+Fx=0FABcos53.13°+FBEcos57.99°10+FBC=0(13.92)cos53.13°+(13.133)cos57.99°10+FBC=0FBC=5.312kips

Apply equilibrium equation to the joint C:

+Fy=0FCDsin53.13°FCEsin57.99°=0(4.830)sin53.13°FCEsin57.99°=0FCE=4.556kips

Sketch the bar forces produced by the P-system as shown in Figure 1.

FUND. OF STRUCTURAL ANALYSIS-W/ACCESS, Chapter 8, Problem 4P , additional homework tip  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=0Dy(22)+1(16)=0Dy=0.727kips

Summation of forces along y-direction is equal to 0.

+Fy=0Dy+Ay+1=00.727+Ay+1=0Ay=0.273kips

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=00.273+FABsin53.13°=0FAB=0.341kips

+Fx=0FAE+FABcos53.13°=0FAE+(0.341)cos53.13°=0FAE=0.205kips

Apply equilibrium equation to the joint D:

+Fy=00.727+FCDsin53.13°=0FCD=0.909kips

+Fx=0FEDFCDcos53.13°=0FED(0.909)cos53.13°=0FED=0.545kips

Apply equilibrium equation to the joint B:

+Fy=0FABsin53.13°FBEsin57.99°=0(0.341)sin53.13°FBEsin57.99°=0FBE=0.322kips

+Fx=0FABcos53.13°+FBEcos57.99°+FBC=0(0.341)cos53.13°+(0.322)cos57.99°+FBC=0FBC=0.375kips

Apply equilibrium equation to the joint C:

+Fy=0FCDsin53.13°FCEsin57.99°+1=0(0.909)sin53.13°FCEsin57.99°+1=0FCE=0.322kips

Sketch the bar forces FQ produced by the vertical dummy load Cy as shown in Figure 2.

FUND. OF STRUCTURAL ANALYSIS-W/ACCESS, Chapter 8, Problem 4P , additional homework tip  2

Refer Table 1 for vertical displacement of joint C.

(b)

To determine

Find the horizontal displacement of joint C.

(b)

Expert Solution
Check Mark

Answer to Problem 4P

The horizontal deflection at joint C (δCx) is 0.269in._.

Explanation of Solution

Given information:

Area of members AB, BC, and CD are 1in.2 and area of members AE, ED, BE, and CE are 0.25in.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=0.363kips

Summation of forces along y-direction is equal to 0.

+Fy=0Dy+Ay=00.363+Ay=0Ay=0.363kips

Summation of forces along x-direction is equal to 0.

+Fx=0Ax=1kip

Find the member forces using method of joints:

Apply equilibrium equation to the joint A:

+Fy=00.363+FABsin53.13°=0FAB=0.455kips

+Fx=0FAE+FABcos53.13°=0FAE+(0.455)cos53.13°1=0FAE=0.727kips

Apply equilibrium equation to the joint D:

+Fy=00.363+FCDsin53.13°=0FCD=0.455kips

+Fx=0FEDFCDcos53.13°=0FED(0.455)cos53.13°=0FED=0.273kips

Apply equilibrium equation to the joint B:

+Fy=0FABsin53.13°FBEsin57.99°=0(0.455)sin53.13°FBEsin57.99°=0FBE=0.429kips

+Fx=0FABcos53.13°+FBEcos57.99°+FBC=0(0.455)cos53.13°+(0.429)cos57.99°+FBC=0FBC=0.5kips

Apply equilibrium equation to the joint C:

+Fy=0FCDsin53.13°FCEsin57.99°=0(0.455)sin53.13°FCEsin57.99°=0FCE=0.492kips

Sketch the bar forces FQ produced by the horizontal dummy load Cx as shown in Figure 3.

FUND. OF STRUCTURAL ANALYSIS-W/ACCESS, Chapter 8, Problem 4P , additional homework tip  3

Refer Table 1 for horizontal displacement of joint C.

(c)

To determine

Find the horizontal displacement of joint D.

(c)

Expert Solution
Check Mark

Answer to Problem 4P

The horizontal deflection at joint D (δDx) is 0.066in._.

Explanation of Solution

Given information:

Area of members AB, BC, and CD are 1in.2 and area of members AE, ED, BE, and CE are 0.25in.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=1kip

Find the member forces using method of joints:

Apply equilibrium equation to the joint A:

+Fy=01+FAB=0FAB=1kips

Apply equilibrium equation to the joint D:

+Fy=01FED=0FED=1kips

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.

FUND. OF STRUCTURAL ANALYSIS-W/ACCESS, Chapter 8, Problem 4P , additional homework tip  4

Find the vertical deflection at joint C (δCy) using the relation:

(1kips)(δCy)=FPFQLAE

Find the horizontal deflection at joint C (δCy) using the relation:

(1kips)(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.)
CxCyDxCxCyDx
AB11013.9200.4550.34100.0760.0570
BC1105.3120.5000.37500.0320.0240
CD1104.8300.4550.90900.0260.0530
DE0.25112.8980.2730.54510.0420.0830.153
EA0.25111.6480.7270.20510.0630.0180.087
EB0.25913.1330.4290.32200.2550.1910
EC0.2594.5560.4290.32200.0890.0660
      δP=FQFPLAE0.2690.3640.066

Refer Table 1.

The vertical deflection at joint C (δCy) is 0.364in._.

The horizontal deflection at joint C (δCx) is 0.269in._.

The horizontal deflection at joint D (δDx) is 0.066in._.

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