Fundamentals of Structural Analysis
Fundamentals of Structural Analysis
5th Edition
ISBN: 9780073398006
Author: Kenneth M. Leet Emeritus, Chia-Ming Uang, Joel Lanning
Publisher: McGraw-Hill Education
Question
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Chapter 15, Problem 1P
To determine

Calculate the horizontal and vertical components of deflection at joint 1 by solving the required equations of equilibrium.

Expert Solution & Answer
Check Mark

Answer to Problem 1P

The horizontal deflection at joint 1 is Δx=96LAE_.

The vertical deflection at joint 1 is Δy=172LAE_.

Explanation of Solution

Apply the sign conventions for the 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 ().

Calculation:

Refer to the given Figure.

Resolve the inclined load of 80 kN in joint 1 into horizontal and vertical component.

Horizontal=80(35)                 =48 kNVertical=80(45)             =64 kN

Sketch the Free Body Diagram of the structure into a number of basic cases as shown in Figure 1.

Fundamentals of Structural Analysis, Chapter 15, Problem 1P

Refer to Figure 1.

Calculate the values of cosϕx and sinϕx for the bars as shown below.

Barcosϕxsinϕx
110
23545

Use Equilibrium equations.

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

+Fx=0K11Δx+K12Δy=48        (1)

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

+Fy=0K21Δx+K22Δy=64        (2)

Calculate the stiffness coefficients due to the unit horizontal and vertical displacements as shown below.

K11=AELcos2ϕx=AEL(12+(35)2)=34AE25L

K21=AELcosϕxsinϕx=AEL(1×0+(35)(45))=12AE25L

K12=AELsinϕxcosϕx=AEL(1×0+(35)(45))=12AE25L

K22=AELsin2ϕx=AEL(0+(45)2)=16AE25L

Solve Equations (1) and (2) to get the values of Δx and Δy as shown below.

34AE25LΔx+(12AE25L)Δy=4834Δx12Δy=1,200LAE(12AE25L)Δx+16AE25LΔy=6412Δx+16Δy=1600LAE

Δx=96LAEΔy=172LAE

Therefore, the horizontal deflection at joint 1 is Δx=96LAE_ and the vertical deflection at joint 1 is Δy=172LAE_.

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