MSE 3300-Lecture Note 09-Chapter 06 Mechanical Properties of Metals 1
Transcript of MSE 3300-Lecture Note 09-Chapter 06 Mechanical Properties of Metals 1
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MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -
Lecture 9. Mechanical Properties
of Metals (1)Learning Objectives
After this lecture, you should be able to do the following:
1. Define engineering stress and strain.
2. Given an engineering stress–strain diagram, determine (a) the
modulus of elasticity, (b) the yield stress, and (c) the tensile strength and
(d) estimate the percentage elongation.
Reading
• Chapter 6: Mechanical Properties of Metals (6.1–6.5)
Multimedia• Tensile tests: https://www.youtube.com/watch?v=ZwTF_-JZgt8;
https://www.youtube.com/watch?v=67fSwIjYJ-E;
https://www.youtube.com/watch?v=K28WiL21Sgs
• Virtual Materials Science & Engineering (VMSE):
http://www.wiley.com/college/callister/CL_EWSTU01031_S/vmse/
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MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -
1. Concepts of Stress and Strain
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Stress–Strain Diagram
Modulus of elasticity, the yield stress, and
the tensile strength
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Type of Loading
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Schematic of how a load produces a deformation (strain): (a) tension, (b)
compression, (c) shear, and (d) torsion
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Tension Tests: Stress-Strain Testing
Fig. 6.3, Callister & Rethwisch 9e.
(Taken from H.W. Hayden, W.G. Moffatt, and J. Wulff, The Structure and Properties of
Materials, Vol. III, Mechanical Behavior , p. 2, John Wiley and Sons, New York, 1965.)
specimen extensometer
• Typical tensile
specimen
Fig. 6.2,
Callister &
Rethwisch 9e.
gauge
length
• Typical tensile test
machine
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• Stress [N/m2 = Pa]
• Strain [dimensionless]
Stress and Strain:
Tension and Compression Tests
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By convention, a compressive
force (thus, stress and strain) is
taken to be negative
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• Shear stress [N/m2 = Pa]
• Shear strain [dimensionless]
Stress and Strain:
Shear and Torsional Tests
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θ γ tan=
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∴ Stress has units:
N/m2 or lbf /in2
Engineering Stress
• Shear stress, τ :
Area, Ao
F t
F t
F s
F
F
F s
τ =F s
A o
• Tensile stress, σ :
original cross-sectional area
before loading
σ = F t A o
2f
2mNor
inlb=
Area, Ao
F t
F t
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• Tensile strain: • Lateral strain:
Strain is always
dimensionless.
Engineering Strain
• Shear strain:
θ
90º
90º - θ y
∆ x γ = Δ x /y = tan θ
e = δ Lo
Adapted from Fig. 6.1 (a) and (c), Callister & Rethwisch 9e.
δ /2
Lowo
- δ eL =
L
wo
δ L /2
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• Simple tension: cable
Note: τ = M / Ac R here.
Common States of Stress
o σ =
F
A
o
τ =F s
A
σ σ
M
M A o
2R
F s A c
• Torsion (a form of shear): drive shaftSki lift (photo courtesyP.M. Anderson)
A o = cross-sectional
area (when unloaded)
F F
τ
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(photo courtesy P.M. Anderson)Canyon Bridge, Los Alamos, NM
o σ = F
A
• Simple compression:
Note: compressivestructure member
(σ < 0 here).(photo courtesy P.M. Anderson)
OTHER COMMON STRESS STATES (i)
A o
Balanced Rock, ArchesNational Park
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• Bi-axial tension: • Hydrostatic compression:
Pressurized tank
σ < 0h
(photo courtesyP.M. Anderson)
(photo courtesy
P.M. Anderson)
OTHER COMMON STRESS STATES (ii)
Fish under water
σ z > 0
σ θ > 0
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2. Elastic Deformation
• Elastic deformation is nonpermanent: when the applied load is released, the
piece returns to its original shape (not breaking atomic bonds).
• Hooke’s Law
E [Pa]: Modulus of elasticity, or Young’s modulus
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Linear elastic deformation Nonlinear elastic deformation
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Elastic means reversible!
Elastic Deformation
2. Small load
F
δ
bonds
stretch
1. Initial 3. Unload
return to
initial
F
δ
Linear-
elastic
Non-Linear- elastic
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Mechanical Properties• Slope of stress strain plot (which is proportional to the
elastic modulus) depends on bond strength of metal
Fig. 6.7, Callister & Rethwisch 9e.
Attraction
Repulsion
r 0
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Elastic Deformation:
Shear Stress and Strain• Elastic deformation is nonpermanent: when the applied load is released, the
piece returns to its original shape.
• Hooke’s Law
G [Pa]: Shear Modulus
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• Shear stress [N/m2 = Pa]
• Shear strain [dimensionless]
θ γ tan=
θ
90º
90º - θ y
∆ x
γ = Δ x /y = tan θ
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Poisson's ratio, ν
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Axial (z) elongation (positive strain)
and lateral (x and y) contractions
(negative strains) in response to an
imposed tensile stress
• Relationship among elastic
parameters for isotropic materials
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Poisson's ratio, ν
• Poisson's ratio, ν :
Units:
E : [GPa] or [psi]
ν : dimensionless
ν > 0.50 density increases
ν < 0.50 density decreases(voids form)
eL
e
-ν
eν = - L
e
metals: ν ~ 0.33
ceramics: ν ~ 0.25
polymers: ν ~ 0.40
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Table 6.1: Elastic and Shear
Moduli and Poisson’s Ratio
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Metals
Alloys
Graphite
Ceramics
Semicond
PolymersComposites
/fibers
E (GPa)
Based on data in Table B.2,
Callister & Rethwisch 9e.
Composite data based on
reinforced epoxy with 60 vol%
of aligned
carbon (CFRE),
aramid (AFRE), or
glass (GFRE)
fibers.
Young
s Moduli: Comparison
109 Pa
0.2
8
0.6
1
Magnesium,
Aluminum
Platinum
Silver, Gold
Tantalum
Zinc, Ti
Steel, Ni
Molybdenum
G raphite
Si crystal
Glass - soda
Concrete
Si nitride Al oxide
PC
Wood( grain)
AFRE( fibers) *
CFRE *
GFRE*
Glass fibers only
Carbon fibers only
A ramid fibers only
Epoxy only
0.4
0.8
2
4
6
10
20
4 0
6 08 0
10 0
200
6008 00
10 001200
400
Tin
Cu alloys
Tungsten
Si carbide
Diamond
PTF E
HDP E
LDPE
PP
Polyester
PS PET
C FRE( fibers) *
G FRE( fibers)*
G FRE(|| fibers)*
A FRE(|| fibers)*
C FRE(|| fibers)*
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Summary
1. Concept of stress and strain
2. Mechanical testing: tensile, compression, shear and
torsional tests
3. Elastic deformation: Modulus of elasticity
4. Poisson’s ratio
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Linear Elastic Properties
• Modulus of Elasticity, E :(also known as Young's modulus)
• Hooke's Law:
σ = E e σ
Linear-elastic
E
e
F
F simpletensiontest
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• Elastic Shear
modulus, G :
τ
G γ
τ = G γ
Other Elastic Properties
simple
torsion
test
M
M
• Special relations for isotropic materials:
2(1 + ν )
EG =
3(1 - 2ν )
EK =
• Elastic Bulkmodulus, K:
pressure
test: Init.vol =V o.
Vol chg.
= ΔV
P
P P P = -K
Δ VVo
P
Δ V
K Vo
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• Simple tension:
δ = FLoE Ao
δ L = - ν Fw oE Ao
• Material, geometric, and loading parameters all
contribute to deflection.
• Larger elastic moduli minimize elastic deflection.
Useful Linear Elastic Relationships
F
Aoδ /2
δ L /2
Lo wo
• Simple torsion:
α = 2MLoπ ro
4G
M = momentα = angle of twist
2r o
Lo