Title: 2' Stress Analysis
12. Stress Analysis
- ENGR 310 Mechanics of Materials
- Fall, 2007
- Tomasz Arciszewski
2Experiments
- Necessary to determine mechanical properties of
materials - Necessary to verify and modify analytical/mathemat
ical models - Computer simulation will never completely replace
experiments
3Tension and Compression Test
- Our focus on tension test
- Objective to determine the relationship between
the average normal stress and average normal
strain in engineering materials - Usually conducted using standard specimens
- Two punch marks establish gauge-length (base)
- Initial measurement
- X-sectional area A0
- Gauge- length L0
- Minimization of bending - ball-and socket-joints
used
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7Loading
- Static - applied very slowly
- Measured and recorded at frequent intervals
8Elongation
- Measured between punch marks
- d L - L0
- Measured using
- a caliper, or an extensometer
9Strain Direct Measurement
Directly measured using electrical resistance
strain gauges
10Strain Direct Measurement
11Stress-Strain Diagram
- Product of a tension or compression test
- Graphical representation of a the relationship
between average normal stress and average normal
strain is called the stress-strain diagram
12Conventional Stress-Strain Diagram
- Nominal (engineering) stress applied load P
divided by the original x-sectional area A0 - ? P/ A0
- Nominal (engineering) strain
- ? ? /L0
- Conventional stress-strain diagram is for nominal
stress and nominal strain
13Conventional Stress-Strain Diagram
- Produced from a tension test
- Static loading
- Mild, low-carbon structural steel (0.2 carbon
content)
14Major Behavior Types
- Elastic behavior - no permanent/plastic
deformations occur after unloading - Plastic behavior - permanent/plastic deformations
occur after unloading - Yielding - relatively constant stresses
- Strain hardening - further stress increase
- Necking - nominal stress decrease
15Elastic Behavior
- occurs when after unloading the specimen comes
back to its initial shape with no plastic
deformations - Proportional limit ? pl is the maximum stress
when the stress-strain relationship is still
linear (proportional) - Elastic limit ?e is the maximum stress when
specimen still retains its initial shape after
unloading
16Plastic Behavior
- occurs when the specimen exhibits
permanent/plastic deformations after unloading
17Yielding and Yield Point
- A type of plastic behavior when the specimen
undergoes deformations under a relatively
constant stress, called yield stress, or stress
changes within the range between upper yield
point and lower yield point
18Strain Hardening
- A type of plastic behavior which occurs after
yielding and the further strain increases are
accompanied by stress increases - Ultimate stress - the maximum nominal stress
recorded during the test
19Necking
- A type of plastic behavior which occurs after
strain hardening, the nominal stress decreases
while strain is still growing - It is localized in the central part of specimen
- Fracture stress - the nominal stress associated
with the fracture of the specimen -
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22True Stress-Strain Diagram
- Conventional diagram is related to the initial
x-sectional area and it has decreasing stress
paradox - True diagram is related to the actual x-sectional
area and it reflects actual normal stresses
(raising)
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24Mild Steel Stress-Strain Diagram
- Mild steel, 0.1 - 0.2 carbon content
- Both upper and lower yield points occur
- Plastic shelf show in light color for an
exaggerated strain scale - Foundation for plastic analysis and design of
steel structures
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26Carbon Content versus Yield Point
27Yield Point Offset Method
28Ductile Materials
- Undergo large deformations before rupture
- Structural, mild steel
- Ductility measures
- Percent elongation (Lf - L0)/L0 100
- (35-40 for mild steel)
- Percent reduction of area (A0 - Af)/A0 100
- (about 60 for mild steel)
29Brittle Materials
- Little or no yielding before fracture
- Small deformations before fracture
- Cast iron, plastics, concrete
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34Behavior various Factors
- Material behavior changes
- Various factors
- Carbon content for steel
- Temperature for steel, plastics
- Aging
- Loading speed
- Radiation (plastics)
- Loading/unloading history
35Ductile Material Fracture Bowl
36Temperature Impact
37Loading Speed Impact
- 500 C degrees
- Left - high speed
- Right - static loading
38Creep Fracture Various Conditions
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41Hookes Law
- Robert Hooke, 1676
- It describes a linear relationship between stress
and strain in within a part of elastic region - ? ? E
- ? - normal stress
- ? - normal strain
- E - the constant of proportionality
42Constant of Proportionality
- Modulus of elasticity
- Youngs modulus
- Unit - force per area
- Slope of the stress-strain line
- 29 103 ksi for steel
43Hookes Law for Shear
- ? G
- - shear stress
- - shear strain
- G - shear modulus, modulus of rigidity, modulus
in shear
44Poissons Ratio
- S.D. Poisson, French, early 1800s
- Axial loading
- Isotropic material
- Elongation/contraction in one direction is
accompanied by a contraction/elongation in a
transverse direction - Approximately 0.29 for steel
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47Poissons Ratio
- ? absol. value of (?transverse/ ?longitudinal)
-
48Relationship among E, ? and G
- G E / (2(1 ?))
- G - modulus in shear
- E - Youngs modulus
- ? - Poissons coefficient
49Axial Loading Elongation/Shortening
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51Axial Loading Elongation/Shortening
- ? ? E
- ? ?/E P/(AE)
- ?l ?l (Pl)/(AE)
52Principle of Superposition
- Fundamental concept in structural analysis and
design - Resultant stress or displacement at the point can
be - determined considering separately various
component - loads and adding stresses or displacements caused
by - them
53Principle of Superposition Requirements
- The loading must be linearly related to the
stress - or displacement that is to be determined
- The loading must not significantly change
- the original geometry or configuration of the
member - or structure
54Thermal Elongation
- Temperature changes in materials cause
deformations and stresses (in statically
indeterminate structures) - A linear relationship is assumed
- ?T ? ?T L
- ? - linear coefficient of thermal expansion (1/C
degree, 1/K degree) - ?T - temperature change
- L - initial length
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