mechanical properties Flashcards

1
Q

engineering/normal stress

A

force/area =F/A = sigma

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2
Q

engineering/normal strain

A

change in length/ original length =l-lo/lo= epsilon

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3
Q

young’s modulus

A

E= stress/strain

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4
Q

hookes law

A

stress=E*strain

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5
Q

typical E for metals

A

~70Gpa-200GPa

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6
Q

typical E for ceramics and glass

A

~70Gpa -400GPa

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7
Q

typical E for polymers

A

~0.5-8Gpa

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8
Q

typical E for diamonds

A

~1150GPa

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9
Q

Poisson’s ratio

A

measure of contraction perpendicular to applied stress
as component gets longer it gets thinner
Ratio=fractional lateral contraction/fractional longitudinal extension

v= - transverse change/ longitudinal change

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10
Q

typical v for metals

A

~0.3-0.35 (1/3 assumed)

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11
Q

typical v for ceramics and glass

A

0.15-0.3

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12
Q

typical v for rubber

A

~0.5 in compressible

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13
Q

typical v for cork

A

0

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14
Q

Shear stress

A

F/A = tau

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15
Q

shear strain

A

gamma = radians of movement

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16
Q

shear modulus

A

G= tau/gamma

Shear stress/shear strain

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17
Q

volume-metric strain

A

change in vol/ og vol

18
Q

bulk modulus

A

pressure/ vol strain

B= - P/(deltaV/V)

19
Q

3 normal stresses

A

sigma 11 , sigma 22, sigma 33

20
Q

3 shear stresses

A

sigma 12, sigma 13, sigmas 23

21
Q

equal stresses

A

sigma 21=12
31=13
23-32

22
Q

moduli

A

6 indie components of stress at a point
6 indie components of strain at a point

6x6=36 moduli to related stress to strain
but with symmetry there is 21 moduli to relate stress to strain

23
Q

isotropic materials - mechanical properties

A

uniform in all directions eg glass

only need 2 moduli to relate stress to strain

24
Q

equi fro stress 11

A

stress11= 1/E [strain11-v(strain22+strain33) ]

same for other numbers

25
Q

equi for shear stress 12

A

stress12 = strain 12/ G

same for other numbers

26
Q

equis relating G B E and V

A

G=E/(2(1+v))

B=E/(3(1-2v))

27
Q

equi for true stress

A

true stress =ln(1+strain) only until necking happens

true stress = (1+strain)stress

28
Q

power law hardening

A

true stress = K true strain^n

29
Q

uniform true strain

A

epsilon u= n

30
Q

ultimate tensile strength

A

stress u = stress t /exp(strain t) = (Kn^n)/exp(n)

31
Q

tensor form uniaxial stress

A

stress 0 0
0 0 0
0 0 0

32
Q

tensor form hydrostatic pressure

A

-p 0 0
0 -p 0
0 0 -p

33
Q

tensor form biaxial stress

A

stress 1 0 0
0 stress2 0
0 0 0

34
Q

tensor form pure shear

A

0 stress12 0
stress12 0 0
0 0 0

35
Q

tensor form plane stress

A

stress11 stress12 0
stress12 stress22 0
0 0 0

36
Q

conventions for stress analysis

A

normal stress tension is +ve

shear stress clockwise is +ve

37
Q

assumptions for stress analysis

A
stresses are 
  -in equilibrium 
  -static 
materials are 
  -isotropic 
  -linear elastic 
deflections are small
38
Q

angled plane - forces and area

A

normal force =Fcos a
shear force = Fsin a
Area = A/cos a

39
Q

angled normal stress

A

stress n =Fcos a/(A/cos a) = stress*cos a^2

40
Q

angled shear stress

A

stress s = Fsin a /(A/cosa)= stress* sin a* cos a

41
Q

von mises yield criterion

A

maximum sistortion energy
(stress1-stress2)^2 +(stress3-stress1)^2 +(stress2-stress3)^2 =2stressys^2

stress1^2 + stress3^2 -stress1stress3 =stressys^2

42
Q

tresca yield criterion

A

stressys= stress1 - stress3

max shear stress
stressxymax = (stress1-stress3)/2