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Truss Analysis for Engineering Students

This document provides a summary of a tutorial on truss analysis using the method of sections. [1] It outlines the procedure for using the method, which involves drawing a free body diagram of the entire truss, selecting a section to cut members, then drawing a free body diagram of the cut portion. [2] Equations of equilibrium are then used to solve for internal forces. [3] Several examples are provided to demonstrate solving for forces in various truss members.

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Deepthi Reddy
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0% found this document useful (0 votes)
102 views13 pages

Truss Analysis for Engineering Students

This document provides a summary of a tutorial on truss analysis using the method of sections. [1] It outlines the procedure for using the method, which involves drawing a free body diagram of the entire truss, selecting a section to cut members, then drawing a free body diagram of the cut portion. [2] Equations of equilibrium are then used to solve for internal forces. [3] Several examples are provided to demonstrate solving for forces in various truss members.

Uploaded by

Deepthi Reddy
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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CIVE1187 Statics

Week 8 Tutorial

Truss Analysis - Section Method

Jie Li

Jie Li 1
The Method of Sections
• Used to determine the loadings within a body
• If a body is in equilibrium, any part of the body is in
equilibrium
• To find forces within members, an imaginary section is
used to cut each member into 2 and expose each
internal force as external
The Method of Sections
Procedure for Analysis
Free-Body Diagram
• Decide the section of the truss
• Determine the truss’s external reactions
• Use equilibrium equations to solve member forces at
the cut session
• Draw FBD of the sectioned truss which has the least
number of forces acting on it
• Find the sense of an unknown member force

Equations of Equilibrium
• Summed moments about a point
• Find the 3rd unknown force from moment equation
Q1
Determine the force in members GE, GC, and BC of the truss.
Indicate whether the members are in tension or compression.

Ax
Ay Dy
Draw FBD of the entire truss

   Fx  0; 400 N  Ax  0  Ax  400 N
 M A  0;  1200 N (8m)  400 N (3m)  D y (12m)  0  D y  900 N
   Fy  0; Ay  1200 N  900 N  0  Ay  300 N
Choose section a-a since it cuts through the 3 members

5m
sin  = 3/5
 

Draw FBD for the section portion

 M G  0;  300 N (4m )  400 N (3m)  FBC (3m)  0  FBC  800 N (T )

 M C  0;  300 N (8m )  FGE (3m )  0  FGE  800 N (C )


3
   Fy  0; 300 N  FGC  0  FGC  500 N (T )
5
Q2 Determine the force in members BC, HC, and HG of
the bridge truss, and indicate whether the members are in
tension or compression.

FBD

Jie Li 6
Support Reactions :
E
ME = 0

18(3) + 14(6) + 12(9) – Ay(12) = 0


Ay = 20.5 kN

MC = 0 -FHG(3) + 12(3) - 20.5(6) = 0

FHG = - 29.0 kN (C) H FHG

MH = 0 3m
FBC(3) – 20.5(3) = 0 45o
FHC
FBC = 20.5 kN (T)
FBC C
Fy = 0; 20.5 – 12 – FHC sin 45° = 0 3m 3m
12 kN
FHC = 12.0 kN (T) Ay=20.5 kN
7
Q3 Determine the force in members EI and JI of the truss
which serves to support the deck of a bridge. State if these
members are in tension or compression.

Jie Li 8
FEF
FEI

Gy

FJI

+ MA = 0 - 40(3) - 80(3x2)- 50(3x5) + Gy(3x6) = 0


Gy = 75 kN

+ ME = 0 –50(3) + 75(6) – FJI(4) = 0


FJI = 75 kN (T)

+↑ Fy = 0; 75 - 50 + FEI = 0
FEI = - 25 kN (C ) 9
Q4 Determine the force in members BC, CG, and GF of
the Warren truss. Indicate if the members are in tension or
compression.

Ax

Ay Ey

+ Fx = 0; Ax= 0
+ ME = 0 6(6) + 8(3) – Ay(9) = 0, Ay = 6.667 kN
10
+ MC = 0
FGF(3 sin 60°) + 6(1.5) – 6.667(4.5) = 0

FGF = 8.08 kN (T)

+ MG = 0

- FBC(3 sin 60°) – 6.667(3) = 0

FBC = - 7.70 kN (C)

+↑ Fy = 0; 6.667 – 6 + FCG sin 60° = 0

FCG = - 0.770 kN (C)


11
Q5 Determine the force in members IC and CG of the truss
and state if these members are in tension or compression.
Also, indicate all zero-force members.

AB, BC, CD, DE, HI,


and GI are all zero-
force members.

+ Fx = 0; Ax= 0
Ax
+ ME = 0

6(1.5) + 6(3) – Ay(1.5x4) = 0


Ay
Ay = 4.5 kN

Jie Li 12
3m FIC cos()
FBC = 0
 sin = 3/5 B FIC sin()
5m cos = 4/5  C
FIC

4m I
FIG=0

A
FHG G
Ay= 4.5 kN 6 kN

+ MG = 0 - 4.5 (3) - FIC (3/5)(4) = 0 FIC = - 5.62 kN (C)

Joint C + Fx = 0; 5.62 sin  + FCJ sin  = 0


FCJ = - 5.62 kN (C)
0 0
 
+↑ Fy = 0; (4/5)5.625 + (4/5)5.625 - FCG = 0
5.62 kN FCJ
FCG FCG = 9 kN (T)
13

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