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1 Announcements Mid-term grades should be up on WebCT tomorrow. THANK YOU for your work in taking the exam. PLEASE be patient! The actual content of the exam will be reviewed in the tutorials this week. WE WILL DO A NEEDS ASSESSMENT (survey) once the grades are out. Welcome to the second half of the course. Moving along to PROPERTIES What was the first half?

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1

Announcements

• Mid-term grades should be up on WebCT tomorrow. – THANK YOU for your work in taking the exam.– PLEASE be patient!– The actual content of the exam will be reviewed in the

tutorials this week.• WE WILL DO A NEEDS ASSESSMENT (survey) once the

grades are out.• Welcome to the second half of the course.

– Moving along to PROPERTIES– What was the first half?

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Materials

• Handle these materials• Find adjectives to describe how the

respond mechanically

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Adjectives

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ADJECTIVES

PROPERTIES

BEHAVIOR

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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 howdo we measure them?

Chapter 6: Mechanical Properties

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EXTREME example

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EXTREME example

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EXTREME example

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Elastic Deformation1. Initial 2. Small load

F

δ

bonds stretch

3. Unload

return to initial

Elastic means reversible!

F

δ

Linear-elastic

Non-Linear-elastic

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Plastic Deformation (Metals)

Plastic means permanent!

F

δlinear elastic

linear elastic

δplastic

1. Initial

F

2. Small load

δelastic + plastic

bonds stretch & planes shear

3. Unload

planes still sheared

δplastic

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∴ Stress has units:N/m2 or lbf/in2

Engineering Stress• Shear stress, τ:

Area, A

Ft

Ft

Fs

F

F

Fs

τ = FsAo

• Tensile stress, σ:

original area before loading

Area, A

Ft

Ft

σ = FtAo

2f

2mNor

inlb=

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• Simple tension: cable

τ

Note: τ = M/AcR here.

Common States of Stress

Ao = cross sectional area (when unloaded)

FF

oσ = F

A

oτ =

FsA

σσ

M

M Ao

2R

FsAc

• Torsion (a form of shear): drive shaft Ski lift (photo courtesy P.M. Anderson)

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(photo courtesy P.M. Anderson)Canyon Bridge, Los Alamos, NM

oσ = F

A

• Simple compression:

Note: compressivestructure member(σ < 0 here).(photo courtesy P.M. Anderson)

OTHER COMMON STRESS STATES (1)

Ao

Balanced Rock, Arches National Park

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• Bi-axial tension: • Hydrostatic compression:

Pressurized tank

σ < 0h

(photo courtesyP.M. Anderson)

(photo courtesyP.M. Anderson)

OTHER COMMON STRESS STATES (2)

Fish under water

σz > 0

σθ > 0

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FLIP CHIPBALL GRID ARRAY

CHIP – Si and interconnects (Cu, Al, other metals)

SOLDER –Pb, Sn other metals

FR4 Board – Cu and insulators (polymers, glasses)

HEATSINK – Al or Cu

ENCAPSULANT –Epoxy, polymers and glasses

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Reliability ModelingPb-Sn Solders

H. Nied and M. OzturkMechanical Engineering

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• Tensile strain: • Lateral strain:

• Shear strain:

Strain is alwaysdimensionless.

Engineering Strain

θ

90º

90º - θy

Δx θγ = Δx/y = tan

ε = δLo

−δεL = L

wo

Adapted from Fig. 6.1 (a) and (c), Callister 7e.

δ/2

δL/2

Lowo

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Stress-Strain Testing• Typical tensile test

machine

Adapted from Fig. 6.3, Callister 7e. (Fig. 6.3 is 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.)

specimenextensometer

• Typical tensile specimen

Adapted from Fig. 6.2,Callister 7e.

gauge length

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MetalsAlloys

GraphiteCeramicsSemicond

Polymers Composites/fibers

E(GPa)

Based on data in Table B2,Callister 7e.Composite data based onreinforced epoxy with 60 vol%of alignedcarbon (CFRE),aramid (AFRE), orglass (GFRE)fibers.

Young’s Moduli: Comparison

109 Pa

0.2

8

0.6

1

Magnesium,Aluminum

Platinum

Silver, Gold

Tantalum

Zinc, Ti

Steel, NiMolybdenum

Graphite

Si crystal

Glass -soda

Concrete

Si nitrideAl oxide

PC

Wood( grain)

AFRE( fibers) *

CFRE*GFRE*

Glass fibers only

Carbon fibers only

Aramid fibers only

Epoxy only

0.4

0.8

2

46

10

20

406080

100

200

600800

10001200

400

Tin

Cu alloys

Tungsten

<100>

<111>

Si carbide

Diamond

PTFE

HDPE

LDPE

PP

Polyester

PSPET

CFRE( fibers) *

GFRE( fibers)*

GFRE(|| fibers)*

AFRE(|| fibers)*

CFRE(|| fibers)*

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Mechanical Properties• Slope of stress strain plot (which is

proportional to the elastic modulus) depends on bond strength of metal

Adapted from Fig. 6.7,Callister 7e.

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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)

εL

ε

εν = − L

ε

metals: ν ~ 0.33ceramics: ν ~ 0.25polymers: ν ~ 0.40

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Next time

• More about what actually happens in the material

• Strengthening (Ch. 7)• More on behavior for specific materials• Failure (Ch. 8)

– Fracture– Creep– Fatigue