l8 more failure v1b
DESCRIPTION
ME 366 Failure Lecture ContinuedTRANSCRIPT
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ME366 Spring 2015 Professor Nathan Salowitz1
ME 366: Design of Machine Elements
Lecture 8: Failure
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ME366 Spring 2015 Professor Nathan Salowitz2
Announcements & Reminders
HW 4 is posted and due Tuesday
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ME366 Spring 2015 Professor Nathan Salowitz3
Agenda
Coulomb-Mohr
Brittle Failure
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ME366 Spring 2015 Professor Nathan Salowitz4
Review
Tresca (maximum shear stress) Calculate principle and max shear stresses
Yield if:
von Mises (distortion energy)
=1
2
2+
2+
2 +
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ME366 Spring 2015 Professor Nathan Salowitz5
Clarification
Why did I do von Mises twice Tuesday? Once with shear only, once with normal stress only?
Example
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ME366 Spring 2015 Professor Nathan Salowitz6
Sty Scy in Some Materials
Grey cast iron
Sty Scy
Magnesium Alloys
Scy Sty
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ME366 Spring 2015 Professor Nathan Salowitz7
Mohr Theory
Perform 3 tests
Uniaxial tension
Uniaxial compression
Pure shear
Plot Mohr's circles
Create failureenvelopes (BCD)
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ME366 Spring 2015 Professor Nathan Salowitz8
Coulomb-Mohr Theory for Ductile Materials
Linearize between uniaxial tension & compression
Define a point O
Similar triangles define
Bs
Cs
Derivation
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ME366 Spring 2015 Professor Nathan Salowitz9
Coulomb-Mohr Ductile Criteria
Yield when:1
3
1
Ultimate failure: 1
3
1
When Syt = Syc = Sy: 1 3
Can calculate =
+
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ME366 Spring 2015 Professor Nathan Salowitz10
Summary of Ductile Failure Theories
Tresca (maximum shear stress)
Conservative
Principle stress based (remember out of plane/0 stress)
Use Ssy if you have it
von Mises (maximum distortion energy)
More accurate
Based on Sy
Coulomb-Mohr
For materials with differing tensile and compressive failure
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ME366 Spring 2015 Professor Nathan Salowitz11
Brittle Materials
Normal failure
More common to have Sut Suc Brittle materials may not yield so ultimate
properties are common
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ME366 Spring 2015 Professor Nathan Salowitz12
Maximum Normal Stress Theory
1 2 3 Failure when:
1 Sut Or
3 Suc
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ME366 Spring 2015 Professor Nathan Salowitz13
Brittle Coulomb-Mohr
1 2 3 A B & 0
Failure predicted when:
A B 0
1 A 0 B
0 A B
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ME366 Spring 2015 Professor Nathan Salowitz14
Modified Mohr
Recall: =
+similarly: =
+
Modify shear criteria yield when
A B 0
()
1 A 0 B
0 A B
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ME366 Spring 2015 Professor Nathan Salowitz15
Brittle Failure Summary
Maximum normal stress
Simple
Not very accurate
Brittle Coulomb Mohr Conservative
Modified Mohr
Improved precision
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ME366 Spring 2015 Professor Nathan Salowitz16
Selecting a Theory
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ME366 Spring 2015 Professor Nathan Salowitz17
Example
A material is uniaxially tested to failure finding : Sut = 14 MPa and Suc = 120 MPa
The critical element of a part made of this material is in plane stress with x = 0 y = -18 MPa, and xy = 20 MPa
Is failure predicted? What would be the factor of safety
Example
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ME366 Spring 2015 Professor Nathan Salowitz18
Fracture Mechanics
Cracks exist in parts from manufacture & grow during service
Damage tolerant design: Parts can function with cracks/damage up to a certain size
Design such that damage can be detected before failure and part fixed or replaced
Modeled with Linear Elastic Fracture Mechanics
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ME366 Spring 2015 Professor Nathan Salowitz19
Flaw Models
Stress concentration factors
Require knowledge of geometry
Radius of curvature of stress raiser critical
Crack tip approaches 0
Concentration factor approaches infinity
Plastic deformation can compensate
Linear elastic models not applicable
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ME366 Spring 2015 Professor Nathan Salowitz20
Fracture
Relatively brittle materials: fracture without yielding occurring throughout the fractured cross section.
Glass, hard steels, strong aluminum alloys
Ductile materials: yield at predictable loading states
Ductile materials will blunt sharp cracks
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ME366 Spring 2015 Professor Nathan Salowitz21
Fracture Energy
Cracking is fast but not instantaneous
Time is necessary to feed energy form the stress field into crack energy
Crack growth occurs when energy release from applied loading is greater than energy for crack growth
Unstable when:
rate of change of energy release rate relative to crack length > rate of change of crack growth energy
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ME366 Spring 2015 Professor Nathan Salowitz22
Crack Modes
m
Opening TearingSliding
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ME366 Spring 2015 Professor Nathan Salowitz23
Mode 1 Analysis
Stress field on dx dy element at crack tip
=
2cos
21
2
3
2
=
2cos
21 +
2
3
2
=
2
2
2
3
2
= 0 plane stress
= ( + )plane stress
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ME366 Spring 2015 Professor Nathan Salowitz24
Stress Intensity Factor
= Units: MPa or psi
For mode 1 crack
1 =
Rewrite:
=1
2cos
21
2
3
2
=1
2cos
21 +
2
3
2
=1
2
2
2
3
2
= 0 plane stress
= ( + )plane stress
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ME366 Spring 2015 Professor Nathan Salowitz25
Stress intensity factor
=
is the stress intensity modification factor
Tabulated for basic geometries
Critical stress intensity factor / fracture toughness KIc is a material property
Dependent on temperature
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ME366 Spring 2015 Professor Nathan Salowitz26
Coming Up
Fatigue
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ME366 Spring 2015 Professor Nathan Salowitz27
Homework #4 Due 2/24/2015 in class
Reading
Chapter 3 & 4
Homework Assignment
3-81 (20 points)
3-100 (10 points)
3-122 (10 points)
4-17 (10 points)
4-104 (10 points)
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