SLIDE 1 Mechanical Properties of Metals How do metals respond to external loads?
Chapter Outline ►Stress and Strain
- Tension
- Compression
- Shear
- Torsion
► Elastic deformation ► Plastic Deformation
- Yield Strength
- Tensile Strength
- Ductility
- Toughness
- Hardness
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To understand and describe how materials deform (elongate, compress, twist) or break as a function of applied load, time, temperature, and other conditions we need first to discuss standard test methods and standard language for mechanical properties of materials.
Introduction
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Concepts of Stress and Strain (tension and compression)
To compare specimens of different sizes, the load is calculated per unit area.
Engineering stress: σ = F / Ao
F is load applied perpendicular to specimen cross-section; A0 is cross-sectional area (perpendicular to the force) before application of the load.
Engineering strain: ε = (Δl / lo) × 100 %
Δl is change in length, lo is the original length. These definitions of stress and strain allow one to compare test results for specimens of different cross- sectional area A0 and of different length l0. Stress and strain are positive for tensile loads,negative for compressive loads
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SLIDE 9 Types of loading
Torsion Shear Tensile compressive
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SLIDE 22 Hardness (I) Hardness is a measure of the material’s resistance to localized plastic deformation (e.g. dent or scratch) A qualitative Moh’s scale, determined by the ability of a material to scratch another material: from 1 (softest = talc) to 10 (hardest = diamond).
Different types of quantitative hardness test has been designed (Rockwell, Brinell, Vickers, etc.). Usually a small indenter (sphere, cone, or pyramid) is forced into the surface of a material under conditions of controlled magnitude and rate of loading. The depth or size of indentation is measured. The tests somewhat approximate, but popular because they are easy and non-destructive (except for the small dent).
SLIDE 23 Hardness
- Resistance to permanently indenting the surface.
- Large hardness means:
- - resistance to plastic deformation or cracking in
compression.
- - better wear properties.
e.g., 10 mm sphere apply known force measure size
removing load
d
D
Smaller indents mean larger hardness.
increasing hardness
most plastics brasses Al alloys easy to machine steels file hard cutting tools nitrided steels diamond
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– No major sample damage – Each scale runs to 130 but only useful in range 20-100. – Minor load 10 kg – Major load 60 (A), 100 (B) & 150 (C) kg
- A = diamond, B = 1/16 in. ball, C = diamond
- HB = Brinell Hardness
– TS (psia) = 500 x HB – TS (MPa) = 3.45 x HB
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Hardness (II)
SLIDE 27 Both tensile strength and hardness may be regarded as degree of resistance to plastic deformation. Hardness is proportional to the tensile strength – but note that the proportionality constant is different for different materials.
For most steels TS (MPa) = 3.45 x HB
SLIDE 28 Hardness tests are performed more frequently than any
- ther mechanical test for several reasons:
1. Inexpensive and simply performed 2. No special specimen need be prepared 3. Nondestructive type of tests ( a small indentation is the only deformation) 4. Other mechanical properties may be estimated from hardness data.
SLIDE 29 True Stress & Strain
Note: S.A. changes when sample stretched
i T
A F
T
ln
1 ln 1
T T
Adapted from Fig. 6.16, Callister & Rethwisch 8e.
SLIDE 30 Hardening
- Curve fit to the stress-strain response:
T K T
n
“true” stress (F/A) “true” strain: ln(L/Lo) hardening exponent: n = 0.15 (some steels) to n = 0.5 (some coppers)
- An increase in y due to plastic deformation.
large hardening small hardening
y
y 1
SLIDE 31 Variability in Material Properties
- Elastic modulus is material property
- Critical properties depend largely on sample flaws
(defects, etc.). Large sample to sample variability.
– Mean – Standard Deviation
s
n
xi x
2
n 1
1 2
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- Design uncertainties mean we do not push the limit.
- Factor of safety, N
N
y working
Often N is between 1.2 and 4
- Example: Calculate a diameter, d, to ensure that yield does
not occur in the 1045 carbon steel rod below. Use a factor of safety of 5.
Design or Safety Factors
220,000N d2 / 4
N
y working
1045 plain carbon steel: y = 310 MPa TS = 565 MPa F = 220,000N
d L o d = 0.067 m = 6.7 cm
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What are the limits of “safe” deformation?
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Design stress: σd = N*σc where σc = maximum anticipated stress, N is the “design factor” > 1. Want to make sure that σd < σy Safe or working stress: σw = σy/N where N is “factor of safety” > 1. For practical engineering design, the yield strength is usually the important parameter