Lecture 16 ENGR-1100 Introduction to Engineering Analysis.
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Transcript of Lecture 16 ENGR-1100 Introduction to Engineering Analysis.
![Page 1: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/1.jpg)
Lecture 16
ENGR-1100 Introduction to Engineering Analysis
![Page 2: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/2.jpg)
Today Lecture Outline
• Structures:•Trusses •Frames
• Trusses analysis- method of joints• Stability criteria.
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Two important structures types
• Trusses: Structures composed entirely of two force members.
• Frames: Structures containing at least one member acted on by forces at three or more points.
![Page 4: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/4.jpg)
• Plane trusses: lie in a single plane.
• Space trusses: not contained in a single plane and/or loaded out of the structure plane.
Plane Trusses
![Page 5: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/5.jpg)
Assumptions
1) Truss members are connected together at their ends only.
2) Truss members are connected together by frictionless pins.
3) The truss structure is loaded only at the joints.
4) The weight of the member may be neglected.
![Page 6: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/6.jpg)
The Four Assumptions
Truss members are two-force members
F
F
Truss member
F
F
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Straight Members
Forces act along the axis of the member
F
F
Compressive forces tend to
shorten the member.
F
F
Tensile forces tend to elongate the
member.
![Page 8: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/8.jpg)
“Rigid” trusses
“Rigid”- the truss will retain its shape when removed from its support
Simple truss- constructed by attaching several triangles together.
Allows a simple way to check rigidity.
![Page 9: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/9.jpg)
What are we looking for?
The support reaction .
The force in each member.
How many equations are available? How many unknowns?
Each joint- 2 equations
Unknowns- number of members+ support reaction.
![Page 10: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/10.jpg)
Stability Criteria
m=2j-32j- number of equations to be solved.
m- number of members.
3- number of support reaction
m<2j-3 Truss unstable
m>2j-3 Statically indeterminate
![Page 11: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/11.jpg)
Example
m (Number of members) =
m=2j-3
13
j (Number of joints) =
Number of supports=
8
3
![Page 12: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/12.jpg)
Method of Joints
Separate free-body diagrams for:
each member
each pin
Equilibrium equations for each pin:
SF=0
no moment equation
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Example 7-3
Use the method of joints to determine the force in each member of the truss shown in Fig. P7-3. State whether each member is in tension or compression.
![Page 14: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/14.jpg)
Solution
TAB TBD
Joint B---------
TBC
y
x
From a free-body diagram on joint B:
Fx = TBC sin 30º - TAB sin 60º = 0
Fy = - TBC cos 30º - TAB cos 60º - TBD = 0
TCDTAD
TBD
Joint D---------
y
x
From a free-body diagram on joint D:
Fy = TBD - 3000 = 0
TBD = 3000 lb = 3000 lb (T)
TAB = - 1500.0 lb = 1500 lb (c)
TBC = - 2598 lb 2600 lb (c)
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known
TCD
Cy
Joint C---------
TBCy
xFrom a free-body diagram on joint C:
Fx = - TCD - TBCsin 30 = - TCD -(2598) sin 30 = 0
Fx = -TAD + TCD = - TAD + 1299 = 0
From a free-body diagram on joint D:
TCDTAD
TBD
Joint D---------
y
xTAD = 1299 lb = 1299 lb (T)
TCD = 1299 lb = 1299 lb (T)
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Class Assignment: Exercise set 7-4please submit to TA at the end of the lecture
Answer:
TBC=14.1 kN (T)
TAC=5.13 kN (T)
TAB=28.2 kN (C)
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Class Assignment: Exercise set 7-6please submit to TA at the end of the lecture
Answer:
TBD=3.23 kN (C)
TCD=4.62 kN (T)
TAD=0.567 kN (T)
TBC=4 kN (C)
TAB=2.38kN (C)
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Zero Force Members
Member BC and DC are zero force members
Free body diagram on joint C
FBC
FCD
y
x
SFy=0 FCD=0
SFx=0FBC=0
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SFy=0 FBD=0
Free body diagram on joint B
FABFCB
y
x
FBD
Free body diagram on joint D
FAD
FED
y
x
FDC
FAD=0
![Page 20: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/20.jpg)
Example 7-19
The truss shown in figure P7-19 support one side of a bridge; an identical truss supports the other side. Floor beams carry vehicle loads to the truss joints. Calculate the forces in members BC, BG, and CG when a truck weighing 7500 lb is stopped in the middle of the bridge as shown. The center of gravity of the truck is midway between the front and rear wheels.
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Solution
From symmetry: FH = FF
Free body diagram on floor beams
Free body diagram on floor beams FH
Fy = 2FG - 2(3750) + 4(1125) = 0
FG= 1500 lb
GFMG = 2FF (10) – 3750 (6) = 0FF = 1125 lb
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f = tan-1 8/5 = 57.99
= tan-1 5/10 =26.57
= tan-1 8/10 =38.66
Free body diagram on complete truss
ME= Ay (30) -1125 (25) - 1500(15) - 1125(5) = 0
Fx = Ax = 0 Ax = 0
Ay = 1875 lb = 1875 lb
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Free body diagram on joint A
Fx = TAB cos 57.99 + TAH = 0
Fy = TAB sin 57.99 + 1875 = 0
TAB = - 2211 lb 2210 lb (c)
TBH = 1125 lb = 1125 lb (T)
Fy = TBH - 1125 = 0
Free body diagram on joint H
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Free body diagram on joint B
Fx = TBC cos 26.57 + TBG cos 38.66
+ 2211cos 57.99 = 0Fy = TBC cos 26.57 - TBG sin 38.66
+ 2211 sin 57.99 - 1125 = 0
TBC = -1451.2 lb 1451 lb (C)
TBG = 161.31 lb 161.3 lb (T)
Free body diagram on joint C
Fx = TCD cos 26.57 + 1451.2 cos 26.57 = 0
Fy = TCD sin 26.57 - TCG + 1451.2 sin 26.57 = 0
TCD = -1451.2 lb 1451 lb (C)
TCG = 1298.2 lb 1298 lb (T)
![Page 25: Lecture 16 ENGR-1100 Introduction to Engineering Analysis.](https://reader036.fdocuments.net/reader036/viewer/2022081501/56649d015503460f949d3290/html5/thumbnails/25.jpg)
Class Assignment: Exercise set 7-23please submit to TA at the end of the lecture