Lecture 5 elastic region Flashcards

1
Q

tensile testing is

A

fundamental test used to extract key properties of materials

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2
Q

specimens shape in tensile testing and why

A

dogbone shape - ends larger than middle - localize stress into the centre of the piece and not be affected by the gripping of the materiel

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3
Q

how is tensile testing done

A

two dots placed on specimen distance measured this

record the extension in the specimen gives the strain measure forced required gives stress

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4
Q

gauge length is the

A

distance between the two dots during tensile testing

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5
Q

loading occurs

A

via load cell with moving cross head - move top head up specimen clamped between two clamps

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6
Q

other properties measured in tensile testing

A

elongation after fraction - tells us about plastic deformation
gauge length at failure - another measure of ductility

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7
Q

engineering stress strain graph regions

A

elastic region - underneath straight line
uniform plastic region yielding - before UTS
nonuniform plastic region necking after UTS

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8
Q

elastic region

A

pulling bonds slightly then letting material go so it returns to its original shape

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9
Q

yeilding region

A

begin to break bonds between material such that it begins to flow - plastic deformation

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10
Q

necking region

A

localise stresses begin to occur failure

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11
Q

bond strength defines the

A

elastic region allows us to define anumber of elastic modula

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12
Q

what is an inset graph

A

due to sharp rise in stresses with little increase in strain during the elastic region on a normal stress strain graph you can not see the elastic region therefore have smaller graph showing just that region

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13
Q

stress

A

force /area

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14
Q

strain

A

change over length / length

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15
Q

if use original length of sample

A

engineering stress and strain inital length and cross sectional area

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16
Q

tensile stress vs compressive stress

A

just negative tensile materiel gets longer and thinner

compressive makes material get shorter and fatter

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17
Q

shear stress

A

applying force parallel to surface

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18
Q

labelled engineering stress stain curve

A

YMS limit of proportionality (hookes law obeyed to)
offset yield strength UTS
failure strength

19
Q

How a material gets strength

A

all material becomes stressed and strained
eventually once you pull past UTS
local region will exhibit large amounts of strain

20
Q

limit of propotionality

A

point beyond which hookes law is no longer obeyed - force and strain directly proportional straight line

21
Q

Yield stress

A

stress at which yeild stress occurs hard to pinpoint typically use offset yield strength

22
Q

UTS

A

point at which plastic deformation becomes unstable and necking begins peak value of engineering stress strain curve

23
Q

fracture

A

point at which material breaks

24
Q

YMs is

A

stiffness of material (not just YMs affected by shape) makes a material difficult to deform
steels typically 100Gpa
within protional region change in stress/strain can be in comprehension constant for a material

25
most materials follow
linear elastically hookes law region follows same line in loading and unloading some materials follow non linear elasticity hookes law not obeyed but loading and unloading still follow same line - use tangential moduli dont worry not on course
26
steeper the elastic region
greater the YMs stiffer the material diamond very stiff would be steepest 100GPa aluminium 69 GPa
27
Ashby diagram
takes two mechanical properties of a material and plots them against each other
28
Ashby diagram
takes two mechanical properties of a material and plots them against each other typically as you increase density increase YMs - elastomers vary from this density moderate but YMS low
29
poissons ratio
materials change cross section area with length elastic region only normal stress is along length of material goes from lo to lo + x cross section goes from A to smaller value lateral direction
30
poissons ratio equal to
- lateral strain/normal strain (negative sign to indicate it is decreasing
31
poissons ratio typically for metals
.33 for metals 0.25 to 0.35 for most
32
poissons ratio close to zero
as you pull them their cross sectional area doesnt change much
33
shear modulus
resistance to shear stress shearing stress to material to produce shear strain symbol G shear stress = G * change in length parrallel to force / length perpendicular to force stress = modulus * strain
34
bulk modulus
resistance to change in volume due to hydro static loading stress = - Bulk modulus * change in volume/original volume bulk modulus equal to K or B
35
4 key elastic moduli
YMs poissons ratio bulk modulus shear modulus
36
equations to link moduli together E G K/B v
``` if have two can calculate other two E = YMs G = Shear modulus K/B = bulk modulus v = possions ratio ```
37
why are all the moduli related
as all defined by bond between atoms
38
bond stiffness or strength
S can be realted to force that is pulling atoms apart and displacement created
39
Bond stiffness equation
E = S/ao
40
bond stiffness equation related to YMs
F = S *delta(a) Stress = force/area = force* change in atomic spacing/atomic spacing ^2 strain = Change in atomic spacing/original atomic spacing Youngs modulus = Stress/strain = Bond stiffness/original atomic spacing E = S/ao see power point for better explanation
41
YMs dependant on
atomic spacing and bond stiffness, all elastic moduli dependent on each other therefore all dependent on these can relate them all
42
force acting on bond stiffness could also be
temperature due to thermal expansion
43
youngs modulus against bond stiffness graph diagram
covalent > metallic > ionic > hydrogen > van der waals bond covalent bond stiffness high YMs metallic high bond stiffness primary bonds have good bond stiffness and good mechanical properties secondary bonds bond stiffness lower and mechanical properties not as good - may be useful