Course E - Mechanical Behaviours of Materials Flashcards
what is tensile testing, explain the different regions and the graph that is formed
- specimen is stretched
- force and corresponding extension of sample is recorded
- done until failure
1) as material extends, force rises and is linear with extension, in this region all deformation is elastic
2) yield point, from linear/elastic —> non-linear/plastic deformation
3) Ultimate tensile strength, highest point on graph, max force a material can withstand
4) failure
what can we say about unloading from a tensile test
- if the only extension that occurred was in the elastic region then it is all recovered
- any plastic deformation is not recovered but the elastic deformation that had occurred is
what is the limitation with tensile testing
- it is very dependent on the size/shape of the material
define stress, give the equation for (true) stress
stress, σ, is the normal force, F, acting on a surface per unit area, A,
σ = F/A
units = Pa
what is an issue that occurs with stress, what alternative expression can we use for stress
- when under stress, the sample can deform and hence the cross-sectional area that the force acts on can change
- hence we tend to just use engineering stress where the initial cross sectional area is taken
σ(eng) = F / Ao
define strain/ give the expression for (true) strain
- strain, ε, is defined as the relative change in the linear dimension of the material in the direction of the force
δε = δl/l
integrate between limits (li and lo) gives
ε(true) = ln(li/lo)
what is engineering strain, give the expression for it
ε(eng) = li-lo/lo = li/lo -1
define shear stress
shear stress, τ, is the force per unit area parallel to a surface
τ = F/Ao
define shear strain, γ
- to do with the change in shape that occurs under a shear stress
- generally under a shear stress a sample will ‘squish’/ deform
- focusing on one vertex we can note the distance by which the opposite side has shifted, this is Δyo, the side length is xo
γ = Δyo/xo = tan(φ)
define Poisson’s ratio, give the equation for it
- we know that under deformation, the shape of a material changes
- i.e. it elongated parallel to the force
- for a normal stress on z we can say
εx = εy = - v εz
where
v = Poisson’s ratio
- generally (0.2 - 0.5)
what is a stress-strain curve, why do we use them, what does the gradient of the linear part give
- similar to force-extension graph but now it is independent of the material geometry
- it follows the exact same shape as a force- ext. graph but has slightly different features
- yield point –> yield stress σy
- ultimate tensile strength –> ultimate tensile stress, σ(UTS)
- strain to failiure εf = strain at failiure
- gradient of linear part = Young’s Modulus, E
define elastic strain, give the equations linking stress and strain for normal and shear stresses
“In an elastic deformation, any strain in response to stress will be immediately and completely recoverable on removal of the stress”
σ = Eε
τ = Gγ
E = Young’s modulus
G = shear modulus
how can we relate E and G using poisson’s ratio, v
E = 2G(1+v)
how can we calculate the elastic strain energy/work done in elastic strain PER UNIT VOLUME for a material
consider work done as
FδL = σAδL = σALδε = VEε δε
W = ∫(0 to εmax) VEε dε = 1/2 Vεmax^2
so
Wv = 1/2 Eεmax^2 (normal stress)
Wv = 1/2 Gγ^2 (shear stress)
what is the link between the work done per unit volume in elastic deformation and the stress-strain graph
- the work done PER UNIT VOLUME is the area under a stress-strain graph
how can we model bonds/ roughly explain the shape of their potential against bond length graph
- when the atoms are far apart, their binding energy –> 0
- as the atoms approach each other PE decreases, potential well, attractive forces
- Umin = PEmin = equilibrium separation of atoms at 0K
- if atoms are close than the bond length at Umin, ro, then their energy rises/repulsive forces
The shape of the potential can be approximated using the Leonard-Jones potential
U(LJ) = Umin[(ro/r)^12 - 2(ro/r)^6]
DON’T LEARN THIS
give a summary of how we can approximate Young’s moduli of a simple cubic crystal using the Leonard Jones potential
for small displacements from ro we assume its roughly linear so
F = dU/dr
(explains F = kx)
we consider stretching a crystal on [100]
If the crystal is simple cubic then:
- each bond has an area ro^2 perp. to normal stress
σ = F/ro^2 = 1/ro^2 dU/dr
E = dσ/dε = dσ/dr dr/dε = (1/ro^2 d^2U/dr^2 |r = ro) (ro)
E = (1/ro) (d^2U/dr^2 | r = ro)
why do we use composites
- we can combine ceramics and polymers for better properties
- generally ceramics/polymers are stronger as fibres
- these fibres are embedded in a matrix material
- orientation within a plane can be random or aligned
- plies of aligned fibres can be stacked
- greatest reinforcing effect when fibres are aligned parallel but this makes material V anisotropic
how can we do analysis on composites/ what model should we use
we can use a slab model:
- we consider ‘slabs’ of the matrix material and fibre material
- the volumes of the slabs correspond to their true volume fractions
how can we determine/estimate the axial modulus of a composite using a slab model
- consider an axial stress on the slabs, this is where the stress acts on the side faces where both slabs are visible
- Voigt Model
- we assume extension by each slab is equal
σc = σfVf + σmVm = σfVf + σm(1-Vf)
σ = Eε
Ecεc = EfεfVf + Emεm(1-Vf)
we assume εc = εf = εm
so
Ec = EfVf + Em(1-Vm)
- this is a reasonable estimate - it is just a weighted average
how can we determine/estimate the transverse modulus of a composite using a slab model
We use Reuss model:
- we assume equal stress
- this time we consider stress acting on the two faces ‘top and bottom’ where only one of the slabs is visible
εc = εfVf + εm(1-Vf)
ε = σ/E
σc/Ec = σfVf/Ef + σm(1-Vf)/Em
σc = σf = σm
so
Ec = EfEm / (EmVf + Ef(1-Vf))
- this is a poor model, lower bound estimate as it does not consider shielding of areas around fibres by fibres
how is temperature related to kinetic energy
3/2 KT = <1/2mv^2> = avr. Ek
microscopically/ on an atomic level, how can we explain thermal expansion
- due to the asymmetry of the Leonard-Jones potential, we can see by taking the mean ro value at different temperatures that ro increases with temp
- this is done by considering higher Y lines on the U(LJ) graph
macroscopically give the equation for what happens in thermal expansion
εt = α ΔT
α = coefficient of thermal expansion
what can we say about the thermal expansion of materials with stronger/weaker bonds
- materials with strong inter-atomic bonds tend to have a lower α value, and a greater E value, and a deep, sharp U well, so they expand less
- materials with weaker inter-atomic bonds tend to have a higher α value, lower E and a shallower U well, so expand more
what can occur to a bimaterial strip when heated/cooled
- if the two materials have different α values then one will expand more than the other
- this can cause bending if the two strips are bonded together
which sections of a beam are under which sorts of stress when bent, what is the neutral axis
- when a rod is bent, the top is under tension, the bottom is under compression
- at the halfway point, there is a neutral axis where σ, ε = 0
what do we define our radius as when considering the bending of beams
- although θ is constant, arclength changes with height so we define our radius as being to the neutral axis
R = l/θ
l = length of neutral axis
how can we calculate σ(axial) and ε(axial) for a bending beam
- we know the neutral axis represents an undeformed length = l = Rθ
- a deformed length is (R+y)θ
Hence
ε(axial) = ((R+y)θ - Rθ) / Rθ = y/R
σ(axial) = Ey/R
how can we calculate the total bending moment on a beam
we know the force on a cross-sectional area is F = σA = Ey/R bdy
b = base length
dy = infinitesimal height difference
moment = F x perp. dist. to N.A. = Ey^2/R
Total bending moment = E/R ∫(-h/2 to h/2) y^2 b dy
= EI/R
I = second moment of area
what is the equation for beam stiffness
Beam stiffness = Λ = EI
I = second moment of area
what is the equation for the second moment of area, what is it for a rectangular section
I = ∫(on the relevant section) y^2 b(y) dy
for a rectangular section
I = bh^3/12
what is the equation for the moment on a cantilever beam
M = F(L-x) = d^2y/dx^2 EI
what is the equation for the deflection at a point, y for a cantilever beam
Hence what is the equation for max. deflection, δ on a cantilever beam
y = (Fx^2/6EI) (3L-x)
max deflection, δ, occurs where x = L, at end
δ = FL^3 / 3EI
in a perfect crystal, what is the only way in which plastic deformation can occur, what is the relevant equation that would give this
in a perfect crystal, plastic deformation can only occur by whole planes of atoms sliding across each other, a ‘Block slip’ model
this would be given by
τ(crit) = Gb / 2πh
b = interatomic spacing
G = shear modulus
h = planar spacing
what is wrong with the ‘block slip’ model in perfect crystals, what is the actual way in which plastic deformation occurs, what is a good way to think about it
- the ‘block slip’ model very much overestimates max. strength
- doesn’t explain why only certain planes move
- actual mechanism is through movement of defects/dislocations
- once a defect/dislocation has moved through the entire crystal, it appears as though the whole plane as slipped but it actually only requires movement of a few atoms at a time
- this explains the lower yield stresses
- can be thought of as difference between pulling an entire rug and moving a ‘ruck’ through a rug
what are dislocations, how can they be thought of locally
line defects
locally they can be thought of as an ‘extra’ half plane of atoms
what are the two vectors that define a dislocation, define them
1) the line vector, l, separates the slipped and unslipped regions of the crystal
2) the Burgers vector, b, describes the magnitude and direction of the displacement caused by the dislocation
how can we determine a burgers vector through a burgers circuit
1) draw a circuit/ closed loop around the dislocation
2) redraw circuit/ closed loop in a ‘perfect crystal’ (one without the dislocation)
3) this will form a closure failure, vector from finish F, to start, S is generally defined as the burgers vector
what is an edge dislocation, give its features and its formal definition
- the line vector runs along the base of the extra half plane of atoms
- corresponding burgers vector can be made by making a burgers circuit
- the convention for the burgers circuit is clockwise around l and F—>S
“an edge dislocation is defined by b perp. to l”
what is a screw dislocation, give its features and its formal definition
- where part of the crystal has sheared
- hard to visualise but imagining a burgers circuit, if a square path is traversed, the end is directly below the start
“Screw dislocations are defined by b parallel to l”
what is a mixed dislocation, give some of its features
- rarely are dislocations pure edge or pure screw
- b can be neither parallel nor perpendicular to l
- this is a mixed dislocation
- commonly found in dislocation loops
by what process do dislocations move, it is localised?
on what do they move?
- dislocations move in a process called glide
- it is very localised and occurs on a single plane called a slip plane
- it is easiest to visualise in an edge dislocation by considering the extra half plane of atoms ‘moving’ across the crystal as they align with another plane of atoms
- screw dislocations move more through a sort of unzipping process
what can we say about the displacement to a section of the crystal that occurs when a dislocation passes
- once the dislocation passes, atoms initially bonded become displaced by a burgers vector
- slip direction // b
- after the dislocation has passed, the structure is perfect again
what are the two KEY CONDITIONS for dislocation motion
1) “If an applied shear stress has a sufficient component parallel to the burgers vector then slip occurs parallel to the burgers vector and the dislocation moves perpendicular to its line vector”
SUFFICIENT FORCE // b
MOVES ⟂ to l
2) “A dislocation can only move on a crystallographic plane that contains both b and l, these planes are slip planes”
from the definition of a slip plane and screw and edge dislocations, what can we say about the number of slip planes for each type
Edge dislocation:
b ⟂ l, so glide is limited to a single slip plane
Screw dislocation:
b // l, so family of possible slip planes
how can we rationalise the movement of a dislocation loop under stress
- we can consider the movement of specific sections under an applied shear stress
By convention:
- a dislocation should be defined by a single line vector, thus the burgers vector is the same around the whole loop
In reality:
- segments on opposite sides of a dislocation loop are of opposite sense
- so their reaction to an applied shear stress // b is opposire
- thus a dislocation loop will expand or contract when a shear stress τ > τcrit is applied
what is the shear stress required to move a dislocation in an otherwise perfect crystal
- the Peierls- Nabarro stress
τp = 3G exp(-2πw / b)
G = shear modulus
w = dislocation width, the distance over which atoms are significantly displaced from their ideal positions (generally where displacement > b/4)
b = modulus (burgers vector)
what is the work done when a dislocation moves, how can we consider forces acting to do this work
If a dislocation is acted on by τ > τcrit then it moves ⟂ l
- hence we expect work to be done
- we can define a virtual ‘glide’ force (not real but useful to consider)
W = FLd
F = glide force (per unit length)
W = work done
L = length of line of dislocation
d = distance dislocation moves
F = τb (THIS IS IN DATA BOOK)
W = τbLd