mom chapter 3-mechanical properties of materials
TRANSCRIPT
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Chapter Objectives Understand how to measure the stress and strain
through experiments
Correlate the behavior of some engineering materials
to the stress-strain diagram.
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1. Check homework, if any
2. Reading Quiz
3. Applications
4. Stress-Strain diagram5. Strength parameters
6. Poissons ratio
7. Shear Stress-strain diagram
8. Concept Quiz
In-class Activities
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TENSION AND COMPRESSION TEST
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READING QUIZ
1) The modulus of elasticity E is a measure ofthe linear relationship between stress and
strain. The common unit is:
a) kN/mm2
b) MPa
c) GPa
d) All of them
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READING QUIZ (cont)
2) The Poissons ratio, vof commonengineering materials lies in the range:
a) 0 v 1
b) 0 v 0.5
c) -1 v 1
d) -0.5 v 0.5
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APPLICATIONS
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APPLICATIONS (cont)
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STRESS STRAIN DIAGRAM
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Note the critical status for strength specification
proportional limit
elastic limit
yield stress
ultimate stress
fracture stress
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STRENGTH PARAMETERS
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Modulus of elasticity (Hookes Law)
Modulus of Resistance
Modulus of Toughness
It measures the enter areaunder the stress-strain diagram
E
Eu plplplr
2
21
21
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EXAMPLE 1
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The stressstrain diagram for an aluminum alloy that is used
for making aircraft parts is shown in Fig. 319. If a specimen
of this material is stressed to 600 MPa, determine the
permanent strain that remains in the specimen when the load
is released. Also, find the modulus of resilience both before
and after the load application.
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EXAMPLE 1 (cont)
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When the specimen is subjected to the load, the strain is approximately
0.023 mm/mm.
The slope of line OA is the modulus of elasticity,
From triangle CBD,
Solutions
mm/mm008.0
100.7510600 9
6
CDCDCD
BDE
GPa0.75
006.0
450E
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EXAMPLE 1 (cont)
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This strain represents the amount ofrecovered elastic strain.
The permanent strain is
Computing the modulus of resilience,
Note that the SI system of units is measured in joules, where 1 J = 1 N
m.
Solutions
(Ans)MJ/m40.2008.060021
2
1
(Ans)MJ/m35.1006.04502
1
2
1
3
3
plplfinalr
plplinitialr
u
u
(Ans)mm/mm0150.0008.0023.0 OC
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POISSONs RATIO
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long
latv
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EXAMPLE 2
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A bar made of A-36 steel has the dimensions shown in Fig.
322. If an axial force of P = 80kN is applied to the bar,
determine the change in its length and the change in the
dimensions of its cross section after applying the load. The
material behaves elastically.
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EXAMPLE 2 (cont)
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The normal stress in the bar is
From the table for A-36 steel, Est= 200 GPa
The axial elongation of the bar is therefore
Solutions
mm/mm108010200
100.16 66
6
st
zz
E
Pa100.1605.01.0
1080 63
A
Pz
(Ans)m1205.11080 6z zz L
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EXAMPLE 2 (cont)
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The contraction strains in both thexand ydirections are
The changes in the dimensions of the cross section are
Solutions
m/m6.25108032.0 6 zstyx v
(Ans)m28.105.0106.25
(Ans)m56.21.0106.25
6
6
yyy
xxx
L
L
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SHEAR STRESS-STRAIN DIAGRAM
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Strength parameter G Shear modulus of elasticity or the
modules of rigidity
G is related to the modulus of elasticity E and Poissonsratio v.
G
vE
G
12
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EXAMPLE 3
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A specimen of titanium alloy is tested in torsion and the
shear stress strain diagram is shown in Fig. 325a.
Determine the shear modulus G, the proportional limit, and
the ultimate shear stress. Also, determine the maximum
distance dthat the top of a block of this material, shown in
Fig. 325b, could be displaced horizontally if the material
behaves elastically when acted upon by a shear force V.What is the magnitude ofV necessary to cause this
displacement?
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EXAMPLE 3 (cont)
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By inspection, the graph ceases to be linear at pointA. Thus, the
proportional limit is
This value represents the maximum shear stress, point B. Thus the
ultimate stress is
Since the angle is small, the top of
the will be displaced horizontally by
Solutions
(Ans)MPa504u
(Ans)MPa360pl
mm4.0mm50
008.0rad008.0tan dd
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EXAMPLE 3 (cont)
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The shear force Vneeded to cause the displacement is
Solutions
(Ans)kN2700
10075MPa360; V
V
A
Vavg
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CONCEPT QUIZ
1) The head H is connected to the cylinder of acompressor using six steel bolts. If the
clamping force in each bolt is 4000N,
determine the normal strain in the bolts.
Each bolt has a diameter of 5 mm. Ify= 280
MPa and Est = 210GPa, what is the strain ineach bolt when the nut is unscrewed so that
the clamping force is released?
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CONCEPT QUIZ (cont)
a) 0.970
b) 0.203
c) 0.970(10-3)
d) Insufficient information to
determine because the
stress is beyond yield point
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