Materials & Grades

Materials & Grades

Metals

Metals are the most commonly used class of engineering material. Metal alloys are especially common, and they are formed by combining a metal with one or more other metallic and/or non-metallic materials. The combination usually occurs through a process of melting, mixing, and cooling. The goal of alloying is to improve the properties of the base material in some desirable way.

Metal alloy compositions are described in terms of the percentages of the various elements in the alloy, where the percentages are measured by weight.

Ferrous Alloys

Ferrous alloys have iron as the base element. These alloys and include steels and cast irons. Ferrous alloys are the most common metal alloys in use due to the abundance of iron, ease of production, and high versatility of the material. The biggest disadvantage of many ferrous alloys is low corrosion resistance.

Carbon is an important alloying element in all ferrous alloys. In general, higher levels of carbon increase strength and hardness, and decrease ductility and weldability.

Carbon Steel

Carbon steels are basically just mixtures of iron and carbon. They may contain small amounts of other elements, but carbon is the primary alloying ingredient. The effect of adding carbon is an increase in strength and hardness.

Most carbon steels are plain carbon steels, of which there are several types.

Low-Carbon Steel

Low-carbon steel has less than about 0.30% carbon. It is characterized by low strength but high ductility. Some strengthening can be achieved through cold working, but it does not respond well to heat treatment. Low- carbon steel is very weldable and is inexpensive to produce. Common uses for low-carbon steel include wire, structural shapes, machine parts, and sheet metal.

Medium-Carbon Steel

Medium-carbon steel contains between about 0.30% to 0.70% carbon. It can be heat treated to increase strength, especially with the higher carbon contents. Medium-carbon steel is frequently used for axles, gears, shafts, and machine parts.

High-Carbon Steel

High-carbon steel contains between about 0.70% to 1.40% carbon. It has high strength but low ductility. Common uses include drills, cutting tools, knives, and springs.

Carbon Steel Materials Table

The table below provides representative mechanical properties for several common carbon steels.

MaterialConditionYield Strength [ksi]Ultimate Strength [ksi]Elongation %Elastic Modulus [psi]Density [lb/in3]Poisson’s Ratio
AISI 1020Hot Rolled32502529e60.2830.32
Cold Worked60705
Stress Relieved506510
Annealed284830
Normalized345522
AISI 1045Hot Rolled45751529e60.2830.32
Cold Worked80905
Stress Relieved70808
Annealed356520
Normalized487515
ASTM A36 36582129e60.2830.3
ASTM A516Grade 7038701729e60.2830.3
Low-Carbon Steel

Low-alloy steels, also commonly called alloy steels, contain less than about 8% total alloying ingredients. Low- alloy steels are typically stronger than carbon steels and have better corrosion resistance.

Some low-alloy steels are designated as high-strength low-alloy (HSLA) steels. What sets HSLA steels apart from other low-alloy steels is that they are designed to achieve specific mechanical properties rather than to meet a specific chemical composition.

The table below provides representative mechanical properties for several common alloy steels.

MaterialConditionYield Strength [ksi]Ultimate Strength [ksi]Elongation %Elastic Modulus [psi]Density [lb/in3]Poisson’s Ratio
AISI 4130Hot Rolled70902029e60.2830.32
Stress Relieved8510510
Annealed557530
Normalized609020
AISI 4140Hot Rolled901201529.7e60.2830.32
Stress Relieved10012010
Annealed608025
Normalized9012020
ASTM A242 46671830e60.2820.3
ASTM A302Grade A45751529e60.2820.29
Grade C508017
ASTM A514Quenched & Tempered1001101829e60.2830.3
ASTM A517Grade F1001151629e60.2800.29
ASTM A533Class 150801829e60.2820.29
Class 2709016
Class 38310016
ASTM A572Grade 5050651830e60.2830.3
ASTM A588 50701829.7e60.2800.28
ASTM A633Grade E55751829.7e60.2800.28
ASTM A656Grade 5050602029e60.2820.29
Grade 60607017
Grade 70708014
Grade 80809012
Grade 10010011012
ASTM A710Grade A80852029.7e60.2800.3
HY-80 801829.7e60.2800.3
HY-100 1001629.7e60.2840.3
Tool Steel

Tool steels are primarily used to make tooling for use in manufacturing, for example cutting tools, drill bits, punches, dies, and chisels. Alloying elements are typically chosen to optimize hardness, wear resistance, and toughness.

Stainless Steel

Stainless steels have good corrosion resistance, mostly due to the addition of chromium as an alloying ingredient. Stainless steels have a chromium composition of at least 11%. Passivation occurs with chromium content at or above 12%, in which case a protective inert film of chromic oxide forms over the material and prevents oxidation. The corrosion resistance of stainless steel is a result of this passivation.

The table below shows the typical compositions of stainless steels:

ElementAusteniticFerriticMartensitic
Carbon0.03 – 0.25%0.08 – 0.20%0.15 – 1.2%
Chromium16 – 26%11 – 27%11.5 – 18%
Nickel3.5 – 22%
Manganese2%1 – 1.5%1%
Silicon1 – 2%1%1%
Austenitic Stainless Steel

Austenitic stainless steel is the most common form of stainless steel. It has the highest general corrosion resistance among stainless steels. It is also the most weldable of the stainless steels due to its low carbon content. It can only be strengthened through cold work. Austenitic stainless steels are generally more expensive than other stainless steels due to nickel content. Austenitic stainless steels are not magnetic, although ferritic and martensitic stainless steels are. Common applications include fasteners, pressure vessels, and piping.

Ferritic Stainless Steel

Ferritic stainless steel has high chromium content and medium carbon content. It has good corrosion resistance rather than high strength. It generally cannot be strengthened through heat treatment, and can only be strengthened via cold work.

Martensitic Stainless Steel

Martensitic stainless steel has high carbon content (up to 2%) and low chromium content. This higher carbon content is the primary difference between ferritic and martensitic stainless steels. Due to the high carbon content, it is difficult to weld. It can be strengthened through heat treatment. Common applications include cutlery and surgical instruments.

Duplex Stainless Steel

Duplex stainless steel contains both austenitic and ferritic phases. It can have up to twice the strength of austenitic stainless steel. It also has a high toughness, corrosion resistance, and wear resistance. Duplex stainless steel is generally as weldabe as austenitic, but it has a temperature limit.

Precipitation-Hardenable Stainless Steel

Precipitation-hardenable stainless steel can be strengthened through precipitation hardening, which is an age hardening process. These materials have high strength as well as high resistance to corrosion and temperature.

Stainless Steel Materials Table

The table below provides representative mechanical properties for several common stainless steels.

MaterialClassConditionYield Strength [ksi]Ultimate Strength [ksi]Elongation %Elastic Modulus [psi]Density [lb/in3]Poisson’s Ratio
AISI 201AusteniticAnnealed40754028e60.2890.27
AISI 202AusteniticAnnealed40754028e60.2890.27
AISI 302AusteniticAnnealed30754028e60.2890.27
AISI 304AusteniticAnnealed30754028e60.2890.29
AISI 304LAusteniticAnnealed25704028e60.2890.28
AISI 316AusteniticAnnealed30754028e60.2890.26
AISI 316LAusteniticAnnealed25704028e60.2890.26
AISI 405Ferritic 25602029e60.2820.28
AISI 410MartensiticAnnealed40701629e60.2820.28
Quenched & Tempered8010012
AISI 430Ferritic 30602029e60.2820.28
AISI 446FerriticAnnealed40651629e60.2820.28
15-5PHMartensitic precipitation hardenableH9001701901028.5e60.2830.27
H102514515512
H115010513516
17-4PHMartensitic precipitation hardenableH9001701901028.5e60.2820.27
H102514515512
H115010513516
17-7PHSemiaustenitic precipitation hardenableTH1050150177629e60.2760.28
A-286Austenitic precipitation hardenable 951401529.1e60.2870.31
Alloy 2205Duplex Austenitic-Ferritic 65952528.5e60.2870.27
Ferrallium 255Duplex Austenitic-Ferritic 801101528.5e60.2870.27

Cast Iron

Cast iron is a ferrous alloy containing high levels of carbon, generally greater than 2%. The carbon present in the cast iron can take the form of graphite or carbide. Cast irons have a low melting temperature which makes them well suited to casting.

Gray Cast Iron

Gray cast iron is the most common type. The carbon is in the form of graphite flakes. Gray cast iron is a brittle material and its compressive strength is much higher than its tensile strength. The fracture surface of gray cast iron has a gray color, which is how it got its name.

Ductile Cast Iron (Nodular Cast Iron)

The addition of magnesium to gray cast iron improves the ductility of the material. The resulting material is called nodular cast iron because the magnesium causes the graphite flakes to form into spherical nodules. It is also called ductile cast iron. Nodular cast iron has good strength, ductility, and machinability. Common uses include crankshafts, gears, pump bodies, valves, and machine parts.

White Cast Iron

White cast iron has carbon in the form of carbide, which makes the material hard, brittle, and difficult to machine. White cast iron is primarily used for wear-resisting components as well as for the production of malleable cast iron.

Malleable Cast Iron

Malleable cast iron is produced by heat treating white cast iron. The heat treatment improves the ductility of the material while maintaining its high strength.

Cast Iron Materials Table

The table below provides representative mechanical properties for several common cast irons.

MaterialClassConditionYield Strength [ksi]Ultimate Strength [ksi]Elongation %Elastic Modulus [psi]Density [lb/in3]Poisson’s Ratio
ASTM A159Gray Cast IronG1800189.6 – 14e60.2640.26
G25002512 – 15e6
G30003013 – 16.4e6
G35003514.5 – 17e6
G40004016 – 20e6
ASTM A536Ductile Cast IronGrade 60-40-1840601824.5e60.2560.29
Grade 65-45-1245651224.5e60.2560.3
Grade 80-55-065580624.5e60.2560.31
Grade 100-70-0370100324.5e60.2560.3
Grade 120-90-0290120223.8e60.2560.28

Aluminum Alloys

Pure aluminum is soft and weak, but it can be alloyed to increase strength. Pure aluminum has good corrosion resistance due to an oxide coating that forms over the material and prevents oxidation. Alloying the aluminum tends to reduce its corrosion resistance.

Aluminum is a widely used material, particularly in the aerospace industry, due to its light weight and corrosion resistance. Despite the fact that aluminum alloys are generally not as strong as steels, they nevertheless have a good strength-to-weight ratio.

Aluminum alloys are named according to a 4-digit number, where the first number indicates the major alloying element. A processing code follows the 4-digit number, which indicates the condition and treatment of the material.

SeriesMajor Alloying ElementHeat Treatable
1XXXNone (commercially pure)No
2XXXCopperYes
3XXXManganeseNo
4XXXSiliconNo (mostly)
5XXXMagnesiumNo
6XXXMagnesium and SiliconYes
7XXXZincYes
SuffixTreatment
-FAs fabricated
-OAnnealed
-HXCold worked (strain hardened)
-TXSolution heat treated, precipitation hardened

The 2000, 6000, and 7000 series aluminum alloys can all be heat treated, and therefore these can achieve the highest strengths. The other alloys can be strengthened through cold work.

The table below provides representative mechanical properties for several common aluminum alloys.

MaterialConditionYield Strength [ksi]Ultimate Strength [ksi]Elongation %Elastic Modulus [psi]Density [lb/in3]Poisson’s Ratio
Al 2014T6, T6515967710.50.1010.33
Al 2024T440621010.50.10.33
Al 5052H322338910.10.0970.33
Al 5083H116, H32131441010.30.0960.33
H32315612
Al 6061T41626169.90.0980.33
T635388
Al 7075T6, T6516878610.30.1010.33

Nickel Alloys

Nickel alloys have high temperature and corrosion resistance. Common alloying ingredients include copper, chromium, and iron. Common nickel alloys include Monel, K-Monel, Inconel, and Hastelloy.

The table below provides representative mechanical properties for several common nickel alloys.

MaterialConditionYield Strength [ksi]Ultimate Strength [ksi]Elongation %Elastic Modulus [psi]Density [lb/in3]Poisson’s Ratio
Hastelloy C-276Solution annealed411004029.80.3210.28
Inconel 625Grade 1551103029.80.3050.28
Grade 24010030
Inconel 686Grade 1851202029.80.3150.28
Grade 212513520
Grade 315016020
Inconel 718Solution annealed & aged1201502029.40.2970.29
Solution heat treated15018010
Inconel 725Solution annealed40754529.60.30.31
Solution annealed & aged12015020
Monel 400Annealed257035260.3190.32
Hot worked407530
Cold worked, stress relieved508020
Monel K-500Annealed & aged8513020260.3060.32
Cold worked & aged10014015

Copper Alloys

Copper alloys are generally characterized as being electrically conductive, having good corrosion resistance, and being relatively easy to form and cast. While they are a useful engineering material, copper alloys are also very attractive and are commonly used in decorative applications.

Copper alloys primarily consist of brasses and bronzes. Zinc is the major alloying ingredient in brass. Tin is a major alloying element in most bronzes. Bronzes may also contain aluminum, nickel, zinc, silicon, and other elements. The bronzes are typically stronger than the brasses while still maintaining good corrosion resistance.

The aluminum bronze alloys are very hard and have good wearing properties, and so are commonly used in bearing applications. The beryllium copper alloys have good strength and fatigue properties, and good wear resistance when lubricated properly. Beryllium copper is commonly used for springs, bearings, and bushings.

The table below provides representative mechanical properties for several common copper alloys.

MaterialMaterial ConditionYield Strength [ksi]Ultimate Strength [ksi]Elongation %Elastic Modulus [psi]Density [lb/in3]Poisson’s Ratio
70/30 Copper-NickelAnnealed18453021.80.3230.3
Cold worked506510
90/10 Copper-NickelAnnealed15383020.30.3230.3
Cold worked305015
Aluminum Bronze 32851215.50.2690.316
Beryllium CopperSolution heat treated7585818.50.2980.27
Precipitation heat treated1401653
Nickel Aluminum Bronze 632Annealed34901016.70.2740.32

Titanium Alloys

Titanium alloys are light, strong, and have high corrosion resistance. Their density is much lower than steel, and their strength-to-weight ratio is excellent. For this reason, titanium alloys are used fairly commonly, especially in the aerospace industry. One primary downside of titanium alloys is the high cost.

There are three categories of titanium alloys: alpha alloys, beta alloys, and alpha-beta alloys. Alpha alloys do not respond to heat treatment and are instead strengthened through solid-solution strengthening processes. The beta and alpha-beta alloys can be strengthened by heat treatment, primarily through precipitation hardening.

Titanium alloys are identified using the percentages of alloying elements, for example Ti-6Al-4V.

The table below provides representative mechanical properties for several common titanium alloys.

MaterialConditionYield Strength [ksi]Ultimate Strength [ksi]Elongation %Elastic Modulus [psi]Density [lb/in3]Poisson’s Ratio
Commercially PureGrade 240502014.80.1630.34
Ti-5Al-2.5SnAnnealed1101151015.50.1620.31
Ti-6Al-4VGrade 512013010160.160.31
Ti-6Al-4V, ELIGrade 231101201016.50.160.31
Ti-5-1-1-1Grade 328510010160.160.31

Polymers

Polymers are materials that consist of molecules formed by long chains of repeating units. They may be natural or synthetic. Many useful engineering materials are polymers, such as plastics, rubbers, fibers, adhesives, and coatings. Polymers are classified as thermoplastic polymers, thermosetting polymers (thermosets), and elastomers.

Thermoplastic Polymers

The classification of thermoplastics and thermosets is based on their response to heat. If heat is applied to a thermoplastic, it will soften and melt. Once it is cooled, it will return to solid form. Thermoplastics do not experience any chemical change through repeated heating and cooling (unless the temperature is high enough to break the molecular bonds). They are therefore very well suited to injection molding.

Thermosetting Polymers

Thermosets are typically heated during initial processing, after which they become permanently hard. Thermosets will not melt upon reheating. If the applied heat becomes extreme however, the thermoset will degrade due to breaking of the molecular bonds. Thermosets typically have greater hardness and strength than thermoplastics. They also typically have better dimensional stability than thermoplastics, meaning that they are better at maintaining their original dimensions when subjected to temperature and moisture changes.

Elastomers

Elastomers are highly elastic polymers with mechanical properties similar to rubber. Elastomers are commonly used for seals, adhesives, hoses, belts, and other flexible parts. The strength and stiffness of rubber can be increased through a process called vulcanization, which involves adding sulfur and subjecting the material to high temperature and pressure. This process causes cross-links to form between the polymer chains.

Ceramics

Ceramics are solid compounds that may consist of metallic or nonmetallic elements. The primary classifications of ceramics include glasses, cements, clay products, refractories, and abrasives.

Ceramics generally have excellent corrosion and wear resistance, high melting temperature, high stiffness, and low electrical and thermal conductivity. Ceramics are also very brittle materials.

Glass

Glasses are common materials and are seen in applications including windows, lenses, and containers. Glasses are amorphous, whereas the other ceramics are mainly crystalline. Primary advantages of glasses include transparency and ease of fabrication. The base element of most glasses is silica, and other components can be added to modify its properties. Common processes used to form glass include:

  • heating until melting, then pouring into molds to cast into useful shapes
  • heating until soft, then rolling
  • heating until soft, then blowing into desired shapes

Cements

Cements are materials that, after mixing with water, form a paste that then hardens. Because of this characteristic, cements can be formed into useful shapes while in paste form before they harden into rigid structures. Plaster of paris is one common cement. The most common cement is called Portland cement, which is made by mixing clay and limestone and then firing at high temperature. Portland cement is used to form concrete, which is made by mixing it with sand, gravel, and water. It can also be mixed with sand and water to form mortar. Like other ceramics, cements are weak in tension but strong in compression. Cement is very inexpensive to produce, and it used widely in the construction of buildings, bridges, and other large structures.

Clay Products

Clay is a very common ceramic material. It can be mixed with water, shaped, and then hardened through firing at high temperature. The two primary classifications of clay products include structural clay products and whitewares. Structural clay products see applications including bricks, tiles, and piping. Whitewares see applications including pottery and plumbing fixtures.

Refractories

Refractory ceramics can withstand high temperatures and extreme environments. They can also provide thermal insulation. Brick is the most common refractory ceramic.

Abrasives

Abrasive ceramics are hard materials that are used to cut, grind, and wear away other softer materials. Typical properties of abrasives include high hardness, wear resistance, and temperature resistance. Abrasives can either be bonded to a surface (e.g. grinding wheels and sand paper), or can be used as loose grains (e.g. sand blasting). Common abrasives include cemented carbide, silicon carbide, tungsten carbide, aluminum oxide, and silica sand. Diamond is also an excellent abrasive, but it is expensive.

Composites

A composite material is a material in which one or more mutually insoluble materials are mixed or bonded together. The primary classes of composites are particulate composites, fibrous composites, and laminated composites.

Particulate Composites

Particulate composites are created by adding particles of one material to a matrix (the filler material). The particles will typically account for less than 15% of the total material volume. The particles are added to improve upon some shortcoming of the matrix material.

Fibrous Composites

A fibrous composite is a material in which fibers of one material are embedded within a matrix. The fibers carry most of the stress, and the matrix serves to hold the fibers in place and to transmit stress between the fibers.

The fibers can be short and randomly oriented, or they can be long and continuous.

Laminated Composites

Laminated composites are created by combining layers of composite materials. The layers will typically differ in the orientation of the fibers, or they will differ in the material itself. Sandwich materials are common, in which a lightweight material (such as foam or a honeycomb) will be placed in between layers of a strong, stiff material