chapter 2 (part 2)
TRANSCRIPT
LOGO
Chapter 2 (Part 2): Principle of Material Science and
Engineering
BKG3493 GAS SYSTEM MATERIALS &
COMPONENTS
CHAPTER OUTCOMES
At the end of this part, you should be able to:
i) Explain mechanical properties for metals such as stress, strain, elasticity modulus, hardness, toughness, ductility and etc
ii) Explain mechanical properties for other materials
iii) Aware that engineering design should include the safety factor
METALS & ALLOYS Metals are used in engineering for many reasons, but
they generally serve as structural elements.
Alloy is a metal composed of more than one element. An alloy has primary constituent and primary alloying elements.
e.g. (i) carbon steel (CS) - Fe, C, Mn
(ii) Stainless steel (SS) – Fe, Cr, Ni, C, Mn
The simplest questions that a design engineer can ask about a structural material are “ How strong is
it?” “How much deformation must I expected given a certain load?”
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ISSUES TO ADDRESS...
• Stress and strain: What are they and why are they used instead of load and deformation?
• Elastic behavior: When loads are small, how much deformation occurs? What materials deform least?
• Plastic behavior: At what point does permanent deformation occur? What materials are most
resistant to permanent deformation?
• Toughness and ductility: What are they and how do we measure them?
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• Simple tension: cable
Common States of Stress
o
s = F
A s s
Ski lift (photo courtesy
P.M. Anderson)
A o = cross sectional
area (when unloaded)
F F
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(photo courtesy P.M. Anderson) Canyon Bridge, Los Alamos, NM
o
s = F
A
• Simple compression:
Note: compressive structure member
(s < 0 here). (photo courtesy P.M. Anderson)
OTHER COMMON STRESS STATES (i)
A o
Balanced Rock, Arches National Park
ENGINEERING STRESS
s =Ft
Aooriginal area
before loading
Stress has a pressure unit
Tensile stress, s: Shear stress, t:
ENGINEERING STRAIN
• Tensile strain: • Lateral strain:
• Shear strain:
= tan Strain is always
dimensionless.
/2
/2
/2 -
/2
/2
/2
L/2L/2
Lowo
TENSILE TEST
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Basic description of the material obtained (see Figure 6.1)
The load necessary to produce a given elongation is monitored as the specimen is pulled in tension at a constant rate
This test produces a load-versus-elongation curve (see Figure 6.2)
A more general statement about material characteristics is obtained by normalizing the data resulting stress-versus-strain curve
TENSILE TEST
STRESS VS STRAIN-METALS
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0
P
As =
Stress? Strain? Units?
0
l
l
D =
Stress σ= Force/Area
Force is also called load (Newton)
So, σ= N/m2= Pa
Usually stress is presented in MPa
Strain Є = extension/ original length
Є=l2-l1/l1 =mm/mm (dimensionless)
1. Modulus of elasticity 2. Yield strength , YS 3. Tensile strength, TS 4. Ductility 5. Toughness Stiffness? Elastic deformation? Plastic deformation?
(1-5) are the key mechanical properties obtained from tensile
test
STRESS VS STRAIN-METALS
ELASTIC DEFORMATION
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F
bonds
stretch
return to
initial
1. Initial 2. Small load 3. Unload
Elastic means reversible!
PLASTIC DEFORMATION
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1. Initial 2. Small load 3. Unload
Plastic means permanent!
MODULUS OF ELASCITY
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Is the slope of the stress-strain curve in the elastic region
Also known as Young’s modulus
The linearity of the stress-strain curve in the elastic region is a graphical statement of Hooke’s law
( σ = EÎ)
This modulus represents the stiffness of the material – its resistance to elastic strain
At the point that the curve is no longer linear and
deviates from the straight-line relationship, Hooke's Law
no longer applies and some permanent deformation
occurs in the specimen.
YIELD STRENGTH (YS)
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• Stress at which noticeable plastic deformation has occurred.
when ep = 0.002 tensile stress, s
engineering strain, e
sy
ep = 0.002
The yield strength is defined relative to the intersection of the stress-strain curve with a 0.2% offset
YIELD STRENGTH: COMPARISON
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Tensile Strength, TS
• Metals: occurs when noticeable necking starts. • Polymers: occurs when polymer backbone chains are aligned and about to break.
sy
strain
Typical response of a metal
F = fracture or
ultimate
strength
Neck – acts as stress
concentrator
en
gin
eeri
ng
TS
str
ess
engineering strain
• Maximum stress on engineering stress-strain curve.
TENSILE STRENGTH (TS)
TENSILE STRENGTH : COMPARISON
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DUCTILITY, %EL
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Quantified as the percent elongation at failure
%EL =L f Lo
Lo
x100
• Another ductility measure: %AR =
Ao A f
Ao
x100
TOUGHNESS
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• Energy to break a unit volume of material • Approximate by the area under the stress-strain curve.
smaller toughness- unreinforced polymers
Engineering tensile strain, e
Engineering
tensile
stress, s
smaller toughness (ceramics)
larger toughness (metals, PMCs)
TOUGHNESS
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The toughness of an alloy depends on a combination of strength and ductility
CREEP
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Plastic deformation occur at high temperatures, constant load, long time period
HARDNESS
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• Resistance to permanently indenting the surface. • Large hardness means: --resistance to plastic deformation or cracking in compression. --better wear properties.
PROPERTIES OF OTHER MATERIALS
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Ceramics and Glasses
PROPERTIES OF OTHER MATERIALS
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Polymers
Flexural modulus
* Based on the same specimen geometry for ceramics (MOR)
Stress-strain
curves for
polyester
engineering
polymer
SUMMARY
• Stress and strain: These are size-independent measures of load and displacement, respectively.
• Elastic behavior: This reversible behavior often shows a linear relation between stress and strain. To minimize deformation, select a material with a large elastic modulus (E or G).
• Plastic behavior: This permanent deformation behavior occurs when the tensile (or compressive) uniaxial stress reaches sy.
• Toughness: The energy needed to break a unit volume of material.
• Ductility: The plastic strain at failure.
• Stiffness: resistance to elastic strain – represented by E
“Every engineering design must take into
account the safety factor (time 1.2 to 4)”