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You are here: Chapter:2 General physics
Section: 2.2 Mechanical properties of materials
SubSection: 2.2.2 Elasticities and strengths
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2.2.2 Elasticities and strengths
Elastic properties isotropic materials
Listed below are the elastic constants in common use, any two of which are sufficient to define the elastic properties of a
homogeneous isotropic solid. The two fundamental constants are those which relate change of volume and change of shape to
applied stress. They are respectively, the bulk modulus K(as inp= K. V/V) and the shear modulus G.
For many practical purposes, the following constants are commonly used:
Youngs Modulus, or longitudinal elasticity, E.
Poissons ratio, = lateral contraction per unit breadth divided by the longitudinal extension per unit length under an applied
longitudinal stress.
Compressibility, = 1/K.
Longitudinal modulus, M, which is the longitudinal modulus for zero lateral strain and determines the velocity of ultrasonic stress
pulses in solids.
For a homogeneous isotropic solid, the following relations exist between the constants.
(a) G=E
2(1 + )
(b) K=E
3 (1 2)
(c) K=1 EG
3 3(3GE)
(d) M= K+4
G3
The value of Poissons ratio is usually positive and lies between 0 and , but in some cases it may be negative.
Elasticities of metals and alloys
Material
20 C
E
GPa
G
GPa
K
GPa
Aluminium . . . . . 70.3 26.1 0.345 75.5
Bismuth . . . . . . 31.9 12.0 0.330 31.3
Cadmium . . . . . 49.9 19.2 0.300 41.6
Chromium . . . . . 279.1 115.4 0.210 160.1
Copper . . . . . . 129.8 48.3 0.343 137.8
Gold . . . . . . . 78.0 27.0 0.44 217.0
Iron (soft) . . . . . 211.4 81.6 0.293 169.8
Iron (cast) . . . . . 152.3 60.0 0.27 109.5
Lead . . . . . . 16.1 5.59 0.44 45.8
Magnesium . . . . . 44.7 17.3 0.291 35.6
Nickel (unmag., soft) . . 199.5 76.0 0.312 177.3
,, ,, hard) . . 219.2 83.9 0.306 187.6
Niobium . . . . . 104.9 37.5 0.397 170.3
Platinum . . . . . 168.0 61.0 0.377 228.0
Silver . . . . . . 82.7 30.3 0.367 103.6
Tantalum . . . . . 185.7 69.2 0.342 196.3
Tin . . . . . . . 49.9 18.4 0.357 58.2
Titanium . . . . . 115.7 43.8 0.321 107.7
Tungsten . . . . . 411.0 160.6 0.280 311.0
Vanadium . . . . . 127.6 46.7 0.365 158.0
Zinc . . . . . . . 108.4 43.4 0.249 72.0
Brass (70 Zn, 30 Cu) . 100.6 37.3 0.350 111.8
Constantan . . . . . 162.4 61.2 0.327 156.4
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Hidurax Special . . . 144.5 54.4 0.333 144.1
Invar (36 Ni, 63.8 Fe, 0.2 C) 144.0 57.2 0.259 99.4
Nickel Silver . . . . 132.5 49.7 0.333 132.0
Steel (Mild) . . . . 211.9 82.2 0.291 169.2
,, ( C) . . . . 210.0 81.1 0.293 168.7
,, ( C hardened) . 201.4 77.8 0.296 165.0
,, Tool||. . . . . 211.6 82.2 0.287 165.3
,, Tool (hardened)|| . 203.2 78.5 0.295 165.2
,, Stainless . . . 215.3 83.9 0.293 166.0
Tungsten Carbide . . 534.4 219.0 0.22 319.0
Approx. value or values for materials of variable composition.
Cu-Ni alloy with Al, Fe and Mn additions.
Approx. %composition: Cu 55, Ni 8, Zn 27.
||Oil hardening non-deforming tool steel of approx. %composition: C 0.98, Mn 1.03, Cr 0.65, W 1.01, V 0.1, remainder Fe.
Approx. %composition: C 0.02, Si 0.5, Mn 0.7, Ni 2, Cr 18, remainder Fe.
Elasticities of glasses
Material
20 C
E
GPa
G
GPa
K
GPa
Glass (Heavy Flint) . . . 80.1 31.5 0.27 57.6
Glass (Crown) . . . . 71.3 29.2 0.22 41.2Quartz (fused) . . . . 73.1 31.2 0.17 36.9
Several values in these tables are taken from Bradfield (1964).
Bulk moduli of elements
Element K
GPa
Element K
GPa
Element K
GPa
Element K
GPa
Aluminium . . 75.5 Chlorine Molybdenum 231.0 Selenium . . 8.3
Antimony . . 42.0 (liq) . . . 1.1 Nickel Silicon . . . 100.0
Arsenic . . 22.0 Chromium . 160.1 (soft) . . 177.3 Silver . . . 103.6
Bismuth . . 31.3 Copper . . 137.8 (hard) . . 187.6 Sodium . . 6.3
Bromine . . 1.9 Gold . . . 217.0 Palladium . 182.0 Sulphur . . 7.7
Cadmium . . 41.6 Iodine . . . 7.7 Phosphorus . Thallium . . 43.0
Caesium . . 1.6 Iron . . . 169.8 (red) . 10.9 Tin . . . . 58.2
Calcium . . 17.2 Lead . . . 45.8 Phosphorus Zinc . . . 72.0
Carbon . . Lithium . . 11.1 (white) . 4.9
(diamond) . 542.0 Magnesium . 44.7 Platinum . 228.0
Carbon Manganese . 118.0 Potassium . 3.1
(graphite) . 33.0 Mercury . . 25.0 Rubidium . 2.5
Bradfield (1964).
Markham (1968).
Bulk moduli of liquids
As the pressure increases, Kincreases. In general a rise in temperature decreases the bulk modulus of a liquid; water, however,
shows a maximum value of Kat about 50 C (see J. H. Poynting and J. J. Thomson (1920) Properties of Matter, London, Charles
Griffin; Bridgman (1949)).
Liquid Temp.
C
K
GPa
Liquid Temp.
C
K
GPa
Acetic acid, 116 atm 20 1.45 Mercury:
Amyl alcohol, 8 atm . 17.7 1.12 837 atm . . . 20 26.2
Benzene, 8 atm . . 17.9 1.10 100200 atm . . 15 30.0
Butyl alcohol, 8 atm . 17.4 1.13 Methyl acetate, 837 atm 14.3 1.04
Butyl alcohol, iso-, 8 atm 17.9 1.03 Methyl alcohol, 37 atm . 14.7 0.97
Carbon bisulphide, 837 atm 15.6 1.16 Olive oil . . . . 20.5 1.60
Carbon tetrachloride . . 20 1.12 Paraffin oil . . . 14.8 1.62
Chloroform, 100-200 atm . 20 1.1 Pentane . . . . 20 0.318
Ether: Petroleum . . . . 16.5 1.46
150 atm . . . 0 0.689 Propyl alcohol, 8 atm . 17.7 1.04
9001000 atm . . 0 1.56 Propyl alcohol, iso-, 8 atm 17.8 0.983
9001000 atm . . 198 0.703 Turpentine . . . 19.7 1.280
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Ethyl acetate, 837 atm . 13.3 0.974 Water:
Ethyl alcohol: 125 atm . . . 15 2.05
1500 atm . . 0 1.32 9001000 atm . . 15 2.75
150200 atm . . 310 0.024 9001000 atm . . 198 1.81
Ethyl bromide, 837 atm . 99.3 0.343 25003000 atm . . 14.2 3.88
Ethyl chloride, 837 atm . 15.2 0.662 Water (sea) . . . 2.32
Glycerine . . . . 20.5 4.03
Elasticities of plastics
All plastics are visco-elastic and consequently the elasticity varies considerably with temperature and strain rate. The table below
gives approximate values at 20 C for slow rates of strain.
Material E
GPa
Material E
GPa
ABS . . . . . . 1.43.1 Polyethylene (high density) . . 0.41.3
Epoxy . . . . . ~3.2 Polyimide . . . . . . . ~3.1
Nylon 6 (cast) . . . 2.43.1 Polymethylmethacrylate (PMMA) 2.43.4
Nylon 6 (moulded) . . 0.83.1 Polypropylene . . . . . . 1.11.6
Nylon 66 . . . . 1.22.9 Polystyrene . . . . . . 2.74.2
Polybenzoxazole . . . ~3.5 Polytetrafluoroethylene (PTFE) 0.4
Polycarbonate . . . 2.4 Polyvinylchloride (PVC) . .
(unplasticised)
2.44.1
Temperature coefficient of elastic constants for a range of materials
Temperature coefficient in
Et= E15{1 - (t15)}
Gt= G15{1 - '(t15)}
At 15C
104for E
'104
for G
Aluminium . . . . 4.8 5.2
Brass . . . . . 3.7 4.6
Copper . . . . . 3.0 3.1
German silver . . . 6.5
Gold . . . . . 4.8 3.3
Iron . . . . . . 2.3 2.8
Phosphor-bronze . . 3.0
Platinum . . . . . 0.98 1.0
Quartz fibre . . . . 1.5 1.1
Silver . . . . . . 7.5 4.5
Steel . . . . . . 2.4 2.6Tin . . . . . . 5.9
Elastic properties anisotropic materials
Anisotropic materials can be either naturally occurring (e.g. wood) or manufactured (e.g. fibre reinforced composites). In general
they are characterised by twenty-one independent constants, but this is reduced to nine for orthotropic materials and five for
transversely isotropic materials. They are frequently planar in form.
The main engineering constants in use for orthotropic composites are:
longitudinal modulus of elasticity, E11
transverse modulus of elasticity, E22
through-thickness modulus of elasticity, E33
longitudinal in-plane shear modulus, G12
longitudinal through-thickness shear modulus, G13
transverse through-thickness shear modulus, G23
major Poissons ratio, 12
minor Poissons ratio, 13
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transverse Poissons ratio, 23
For unidirectionally reinforced composites, 1 = fibre direction in-plane, 2 = transverse to fibre in-plane and 3 = transverse
through-thickness (i.e. perpendicular to plane). For other materials, the directions would be defined by other features, such as the
production length-wise direction. Poissons ratio can be greater than 0.5 for angle-ply or multidirectionally reinforced materials.
Composites with fully unidirectional reinforcement are approximately transversely isotropic materials (i.e. 2 and 3 directions are
equal). The following relations exist in this case:
E33= E22, G13= G12, 13= 12,
and E22= 2(1 + 23)G23
For orthotropic symmetry the following relations exist:
12=
21,
23=
32,
13=
31
E11 E22 E22 E33 E11 E33
Elasticities of woods
All woods are elastically anisotropic and in general there are nine independent elastic constants. The values in the table below are
for some common woods and give the three principal values of Youngs modulus measured along the grain EL, in a radial direction
ERand tangential direction ET(Hearmon, 1948).
WoodRelative
density
EL
GPa
ER
GPa
ET
GPa
Ash . . . . . . . . 0.7 16 1.6 0.9
Balsa . . . . . . . 0.2 6 0.3 0.1
Beech . . . . . . . 0.7 14 2.2 1.1
Birch . . . . . . . 0.6 16 1.1 0.6
Mahogany . . . . . . 0.5 12 1.1 0.6
Oak . . . . . . . . 0.7 11
Walnut . . . . . . . 0.6 11 1.2 0.6
Teak . . . . . . . . 0.6 13
Douglas Fir . . . . . . 0.5 16 1.1 0.8
Scots Pine . . . . . . 0.5 16 1.1 0.6Spruce . . . . . . . 0.40.5 1016 0.40.9 0.40.6
Elasticities of fibre-reinforced plastics full set
Material E11
GPa
E22
GPa
E33
GPa
G12
GPa
G13
GPa
G23
GPa
v12 v21 v23
High Modulus Carbon Fibre/Epoxy
unidirectionally reinforced
specimen 287 7.80 7.75 6.7 6.7 2.5 0.30 0.01 0.55
High Strength Carbon Fibre/Epoxy
unidirectionally reinforced
specimen 172 11.6 11.6 7.8 7.8 3.9 0.36 0.02 0.48
Elastic Constants measured at NPL by the Ultrasonic Technique (Read and Dean, 1978).
Elasticities of fibre-reinforced plastics in-plane properties
Material23 C
E11
GPa
E22
GPa
v12 v21
Injection moulded, discontinuous (long) fibre thermoplastic: glass-fibre/nylon
(30%fibre by volume) 10.6 7.9 0.34 0.22
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Hot compression moulded, sheet moulding (thermoset) compond (SMC): glass
fibre strands/filler/polyester resin (62%fibre + filler by volume) 10.0 9.8 0.30 0.31
Thermoformed (press) moulded, mat + unidirectional fibres/thermoplastic
glass-fibre/polypropylene (18%fibre by volume) 9.2 4.4 0.41 0.22
Autoclaved, unidirectional continuous fibre/thermoset resin: glass-fibre/epoxy
(59%fibre by volume) 47.0 16.4 0.28 0.08
Autoclaved, unidirectional continuous fibre/thermoset resin: carbo-fibre/epoxy
(61%
fibre by volume) 146 9.9 0.30 0.02
Typical values measured at NPL using mechanical test methods (Sims et al., 1993) actual values depend on fibre type,
orientation and distribution, also on resin properties and process route.
Strength properties isotropic materials
The strength properties of many materials are dependent on the rate of loading and the test temperature. This particularly applies
to plastics and glass-fibre reinforced plastics. Generally materials will reach their elastic l imit prior to failure.
Substance Tensile
strength
MPa
Metals
Aluminium (cast) 90100
(rolled) 90150
Brass (66% Cu, 34% Zn) (cast) 150190
" (rolled) 230270
Calcium 4260
Cobalt 260750
Copper (cast) 120170
,, (rolled) 200400
Gun metal (90% Cu, 10% Sn) 190260
Iron (cast) 100230
,, (wrought) 290450
Lead (cast) 1217
Magnesium (cast) 6080
,, (extruded) 170190
Phosphor-bronze (cast) 180280
Steel (castings). 400600
Steel (mild) (0.2% C) 430490
High-carbon spring steel:
(annealed 700770
(tempered) 9301080
(nickel) (5% Ni) 8001000
(nickel-chromium) 10001500
Soft solder 5575
Tin (cast) 2035
Zinc (rolled) 110150
Plastics
Nylon 6 7697
Nylon 66 6283
Polyacetal ~69
Polybenzoxazole 82117
Polycarbonate 5565
Polyethylene 2135
Polyimide 69-104
Polymethylmethacrylate 50-76
Polypropylene 30-40
Polystyrene 34-52
Miscellaneous
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Catgut 420
Glass 3090
Hemp rope 60100
Leather belt 3050
Silk fibre 260
Spider thread 180
Woods:
Ash, beech, oak, teak, mahogany 60110
Fir, pitch-pine 4080 Red or white deal 3070
White or yellow pine 2050
Quartz fibre (fused) ~1000
Wires
Aluminium 200-450
Brass 350-550
Copper (hard-drawn) 400460
,, (annealed) 280-310
Duralumin 400-550 German Silver 460
Gold 200250
Iron (charcoal, hard-drawn 540-620
,, (annealed) 460
Molybdenum 11003000
Nickel 500-900
Palladium 350450
Phosphor-bronze (hard-drawn) 6901080
Platinum 330370
Pt + 10% Rh 630
Silver 290
Steel (ordinary) ~1100
,, (tempered) 1550 ,, (pianoforte, hard-drawn) . 18602330
Tantalum 8001100
Tungsten 15003500
Zirconium (annealed) 260390
,, (hard-drawn) 1000
Along the grain
Strength properties anisotropic materials
The strength properties of anisotropic materials measured in different directions may differ considerably. Differences in strengthscan be higher than those in elastic properties.
Ultimate tensile strength properties of fibre-reinforced plastics in-plane properties. (Sims et al., 1993). Typical values;
actual values depend on fibre type, orientation and distribution; resin properties and process route (NB. 11 = longitudinal
ultimate tensile strength and 22= transverse ultimate tensile strength).
Material
23 C11
MPa
22
MPa
Injection moulded discontinuous (long) glass-fibre/nylon (30%fibre by volume) 148 113
Hot comperssion moulded, sheet moulding material (SMC) glass fibre strands/filler/polyester
resin (62%fibre + filler by volume)
60
59
Thermoformed (press) moulded, mat + unidirectional/thermoplastic glass-fibre/
polypropylene (18%fibre by volume )
143 38
Autoclaved, unidirectional glass-fibre/epoxy (59%fibre by volume) 1139 63
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Autoclaved, unidirectional carbon-fibre/epoxy (61%fibre by volume) 2386 76
References
G. Bradfield (1964) Notes on Applied Science No. 30, Use in Industry of Elasticity with the Help of Mechanical Vibrations, HMSO.
P. W. Bridgman (1949) The Physics of High Pressure, Bell.
J. A. Ewing (1899) Strength of Material, Cambridge University Press.
R. F. S. Hearmon (1948). See also R. F. S. Hearmon, Elasticity of Wood and Plywood, Forest Products Research Special Report No.
7, HMSO.
M. F. Markham (1968) Measurements made at the NPL.
B. E. Read and G. D. Dean (1978) The determination of dynamic properties of polymers and composites, Adam Hilger.
G. D. Sims, W. Nimmo and W. R. Broughton (1993) Data measured at the NPL.
Others sources of data include,
W. Bolton (1989) Engineering Materials Pocket Book, Newnes.
Handbook of Industrial Materials(1992) Elsevier Adv. Tech.
N. A. Waterman and M. F. Ashby (1992) Elsevier Materials Selector, Elsevier Applied Science.
G.Sims
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