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Ultimate tensile strength

From Wikipedia, the free encyclopedia
Maximum stress withstood by stretched material before breaking

Two vises apply tension to a specimen by pulling at it, stretching the specimen until it fractures. The maximum stress it withstands before fracturing is its ultimate tensile strength.

Ultimate tensile strength (also calledUTS,tensile strength,TS,ultimate strength orFtu{\displaystyle F_{\text{tu}}} in notation)[1] is the maximumstress that a material can withstand while being stretched or pulled before breaking. Inbrittle materials, the ultimate tensile strength is close to theyield point, whereas inductile materials, the ultimate tensile strength can be higher.

The ultimate tensile strength is usually found by performing atensile test and recording theengineering stress versusstrain. The highest point of thestress–strain curve is the ultimate tensile strength and has units of stress. The equivalent point for the case of compression, instead of tension, is called thecompressive strength.

Tensile strengths are rarely of any consequence in the design ofductile members, but they are important with brittle members. They are tabulated for common materials such asalloys,composite materials,ceramics, plastics, and wood.

Definition

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The ultimate tensile strength of a material is anintensive property; therefore its value does not depend on the size of the test specimen. However, depending on the material, it may be dependent on other factors, such as the preparation of the specimen, the presence or otherwise of surface defects, and the temperature of the test environment and material.

Some materials break very sharply, withoutplastic deformation, in what is called a brittle failure. Others, which are more ductile, including most metals, experience some plastic deformation and possiblynecking before fracture.

Tensile strength is defined as a stress, which is measured asforce per unit area. In theInternational System of Units (SI), the unit is thepascal (Pa) which is 1 N/m2 or for tensile strength more often a multiple thereof, like megapascals (MPa) or gigapascals (GPa). For some non-homogeneous materials (or for assembled components) it can be reported just as a force or as a force per unit width. AUnited States customary unit ispounds per square inch (lb/in2 or psi). Kilopounds per square inch (ksi, or sometimes kpsi) is equal to 1000 psi, and is commonly used in the United States, when measuring tensile strengths.

Ductile materials

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Figure 1: "Engineering" stress–strain (σ–ε) curve typical of aluminium
  1. Ultimate strength
  2. Yield strength
  3. Proportional limit stress
  4. Fracture
  5. Offset strain (typically 0.2%)
Figure 2: "Engineering" (red) and "true" (blue)stress–strain curve typical ofstructural steel.
  1. Apparent stress (F/A0)
  2. Actual stress (F/A)
()

Many materials can display linearelastic behavior, defined by a linearstress–strain relationship, as shown in figure 1 up to point 3. The elastic behavior of materials often extends into a non-linear region, represented in figure 1 by point 2 (the "yield strength"), up to whichdeformations are completely recoverable upon removal of the load; that is, a specimen loaded elastically intension will elongate, but will return to its original shape and size when unloaded. Beyond this elastic region, forductile materials, such as steel, deformations areplastic. A plastically deformed specimen does not completely return to its original size and shape when unloaded. For many applications, plastic deformation is unacceptable, and is used as the design limitation.

After the yield point, ductile metals undergo a period of strain hardening, in which the stress increases again with increasing strain, and they begin toneck, as the cross-sectional area of the specimen decreases due to plastic flow. In a sufficiently ductile material, when necking becomes substantial, it causes a reversal of the engineering stress–strain curve (curve A, figure 2); this is because theengineering stress is calculated assuming the original cross-sectional area before necking. The reversal point is the maximum stress on the engineering stress–strain curve, and the engineering stress coordinate of this point is the ultimate tensile strength, given by point 1.

Ultimate tensile strength is not used in the design of ductilestatic members because design practices dictate the use of theyield stress. It is, however, used for quality control, because of the ease of testing. It is also used to roughly determine material types for unknown samples.[2]

The ultimate tensile strength is a common engineering parameter to design members made of brittle material because such materials have noyield point.[2]

Testing

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Round bar specimen after tensile stress testing
Aluminium tensile test samples after breakage
The "cup" side of the "cup–cone" characteristic failure pattern
Some parts showing the "cup" shape and some showing the "cone" shape
Main article:Tensile testing

Typically, the testing involves taking a small sample with a fixed cross-sectional area, and then pulling it with atensometer at a constant strain (change in gauge length divided by initial gauge length) rate until the sample breaks. In metals and especially in polymers, the ultimate strength can depend significantly on the strain rate selected for the test.[3]

When testing some metals,indentation hardness correlates linearly with tensile strength. This important relation permits economically important nondestructive testing of bulk metal deliveries with lightweight, even portable equipment, such as hand-heldRockwell hardness testers.[4] This practical correlation helpsquality assurance in metalworking industries to extend well beyond the laboratory anduniversal testing machines.

Typical tensile strengths

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Typical tensile strengths of some materials
MaterialYield strength
(MPa)
Ultimate tensile strength
(MPa)
Density
(g/cm3)
USAF-96 Steel1,3371,7017.85
Steel, structural ASTMA36 steel250400–5507.8
Steel, 10902478417.58
Chromium-vanadium steel AISI 61506209407.8
Steel, 2800Maraging steel[5]2,6172,6938.00
Steel,AerMet 340[6]2,1602,4307.86
Steel, Sandvik Sanicro 36Mo logging cable precision wire[7]1,7582,0708.00
Steel, AISI 4130,
water quenched 855 °C (1,570 °F), 480 °C (900 °F) temper[8]
9511,1107.85
Steel, API 5L X65[9]4485317.8
Steel, high strength alloy ASTMA5146907607.8
Acrylic, clear cast sheet (PMMA)[10]7287[11]1.16
Acrylonitrile butadiene styrene (ABS)[12]43430.9–1.53
High-density polyethylene (HDPE)26–33370.85
Polypropylene12–4319.7–800.91
Steel, stainless AISI 302[13]2756207.86
Cast iron 4.5% C, ASTM A-481302007.3
"Liquidmetal" alloy[citation needed]1,723550–1,6006.1
Beryllium[14] 99.9% Be3454481.84
Aluminium alloy[15] 2014-T64144832.8
Polyester resin (unreinforced)[16]5555 
Polyester and chopped strand mat laminate 30% E-glass[16]100100 
S-Glass epoxy composite[17]2,3582,358 
Aluminium alloy 6061-T62413002.7
Copper 99.9% Cu70220[citation needed]8.92
Cupronickel 10% Ni, 1.6% Fe, 1% Mn, balance Cu1303508.94
Brass200 +5008.73
Tungsten9411,51019.25
Glass, annealed 41[18]2.53
E-Glass1,500 for laminates,
3,450 for fibers alone
2.57
S-Glass4,7102.48
Basalt fiber[19]4,8402.7
Marble152.6
Concrete2–52.7
Carbon fiber1,600 for laminates,
4,137 for fibers alone
1.75
Carbon fiber (Toray T1100G)[20]
(the strongest human-made fibres)
 7,000 fibre alone1.79
Human hair140–160200–250[21]1.32[22]
Bamboo fiber 350–5000.4–0.8
Spider silk (see note below)1,0001.3
Spider silk,Darwin's bark spider[23]1,652
Silkworm silk500 1.3
Aramid fibers (Kevlar orTwaron)2,920-3,000[24]1.44
Aramid fiber impregnated epoxy (Kevlar orTwaron)3,600[24]
UHMWPE[25]24520.97
UHMWPE fibers[26][27] (Dyneema or Spectra)2,300–3,5000.97
Vectran 2,850–3,3401.4
Polybenzoxazole (Zylon)[28]2,7005,8001.56
Wood,pine (parallel to grain) 40 
Bone (limb)104–1211301.6
Nylon, molded, 6PLA/6M[29]75–851.15
Nylon fiber, drawn[30]900[31]1.13
Epoxy adhesive12–30[32]
Rubber16[citation needed] 
Boron3,1002.46
Silicon, monocrystalline (m-Si)7,0002.33
Ultra-puresilica glass fiber-optic strands[33]4,100
Sapphire (Al2O3)400 at 25 °C,
275 at 500 °C,
345 at 1,000 °C
1,9003.9–4.1
Boron nitride nanotube33,0002.62[34]
Diamond1,6002,800
~80,000–90,000 at microscale[35]
3.5
Grapheneintrinsic 130,000;[36]
engineering 50,000–60,000[37]
1.0
Firstcarbon nanotube ropes?3,6001.3
Carbon nanotube (see note below)11,000–63,0000.037–1.34
Carbon nanotube composites1,200[38]
High-strength carbon nanotube film9,600[39]
LimpetPatella vulgata teeth (goethitewhiskernanocomposite)4,900
3,000–6,500[40]
^a Many of the values depend on manufacturing process and purity or composition.
^b Multiwalled carbon nanotubes have the highest tensile strength of any material yet measured, with one measurement of 63 GPa, still well below one theoretical value of 100 GPa.[41] The first nanotube ropes (20 mm in length) whose tensile strength was published (in 2000) had a strength of 3.6 GPa.[42] The density depends on the manufacturing method, and the lowest value is 0.037 or 0.55 (solid).[43]
^c The strength of spider silk is highly variable. It depends on many factors including kind of silk (Every spider can produce several for sundry purposes.), species, age of silk, temperature, humidity, swiftness at which stress is applied during testing, length stress is applied, and way the silk is gathered (forced silking or natural spinning).[44] The value shown in the table, 1,000 MPa, is roughly representative of the results from a few studies involving several different species of spider however specific results varied greatly.[45]
^d Human hair strength varies bygenetics, environmental factors, and chemical treatments.

Typical properties of annealed elements

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Typical properties forannealed elements[46]
ElementYoung's
modulus
(GPa)
Yield
strength
(MPa)
Ultimate
strength
(MPa)
Silicon1075,000–9,000
Tungsten411550550–620
Iron21180–100350
Titanium120100–225246–370
Copper130117210
Tantalum186180200
Tin479–1415–200
Zinc85–105200–400200–400
Nickel170140–350140–195
Silver83170
Gold79100
Aluminium7015–2040–50
Lead1612

See also

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  • Limit load (physics), maximum load that a structure is expected to safely carry in service
    • Safe working load or working load limit, maximum load during normal operations specified in the interests of avoiding failure
  • Ultimate load, figure used in calculations that should hopefully never actually occur

References

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Further reading

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