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Aluminum Sheet Alloys

October 27, 2025
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Steel grades—excluding stainless steels—typically are named after their mechanical performance and production route (cold- or hot-rolled). Names may be based on their deep drawability (CR3, DX54), yield strength (CR210LA, S700MC), tensile strength (SPC340BH, HDT590X) or both (CR330Y590T-DP)

Table 1Aluminum alloys are different. First, automotive OEMs only recently started standardizing their aluminum alloys. The distinction between hot- and cold-rolled usually is not critical. Instead, most alloy nomenclature relates to composition. In North America, the Aluminum Association defines a four-digit code for each alloy (Table 1). These digits often follow the letters AA. Example: alloy AA6016, which may be referred to as EN-AW6016 in Europe, where EN stands for European Norm and AW stands for wrought aluminum. 

Cracking the Code: What Do the Four Digits Mean?

The first of the four digits in the alloy designation indicates the main alloying element, and also provides information about the tempers. In 1xxx-series grades, the last two digits indicate the aluminum percentage. AA1050, then, contains 99.50% Al, while AA1098 contains 99.98% Al. The last two digits do not have any significant meaning in other alloy series (2xxx to 8xxx). AA2014 is the 14th registered alloy in copper-alloyed grades, and AA6014 is the 14th alloy in Mg-Si-alloyed grades.

Table 2The second digit in the alloy designation also tells a story. A zero indicates an original alloy, while any other number indicates some modification of the original alloy. Example: AA5054 is the original 54th alloy in Mg-alloyed aluminum grades, and AA5754 is the 7th modification of the same alloy. 

The four digits may be followed by a letter, which indicates the variation of the alloy. AA6110A, for example, is a variation of AA6110, which itself is a modification of AA6010. Table 2 provides the chemical compositions of these grades, as defined by the Aluminum Association.

How About Mechanical Properties?

Table 3An aluminum alloy’s name does not indicate its strength (yield or tensile), unless the name also includes the temper—indicated by a letter and often followed by one or more numbers. Temper designation provides the processing history and defines the strength-ductility level of the material (Table 3).

It also is critical to note that only 2xxx, 6xxx and 7xxx-series alloys, as well as some 4xxx grades, can be heat treated.

Once we know the alloy and temper, we can refer to several standards (including EN 485-2) to obtain an alloy’s strength value. Fig. 1, for example, provides the stress-strain curve for two aluminum grades (AA 1100-O, one of the softest and most ductile grades, and AA 5754-H111), and for a draw-quality steel for comparison.

Is It Easier or Harder to Form Aluminum, Compared to Steel?

Fig. 1The answer to this question depends on the definition of “easy.” When working with soft tempers of 5xxx or 6xxx aluminum grades, yield and tensile strength are similar to or perhaps less than that of mild steels—it will take less load to bend the aluminum. However, the aluminum sheet will exhibit much more springback than a steel sheet at a similar strength level, as aluminum has one-third the elastic modulus.  Looking at the curves in Fig. 1, it is clear that press-forming aluminum requires less force and energy compared to steel (with the specific grades shown in the figure). 

“Easy to form” might also refer to forming crack-free parts. Aluminum has three major drawbacks when compared to steel: aluminum grades typically have less total elongation; they have negative strain-rate sensitivity (m-value); and they have very low r-values. 

Fig. 2It is assumed—and mostly true—that an alloy with a higher total elongation also has more formability. Thus, one easily can check the graphs in Fig. 2 and say that aluminum is less formable than steel. Now imagine a steel grade with a total elongation similar to that of aluminum. The next property to consider: m-value. When local necking starts, strain rate in the necked area becomes much higher than in its surrounding non-necking area. With a negative strain-rate sensitivity, the necked area would be softer than the surrounding area. As both the strength and cross-sectional area get smaller, we should see fracture very soon after necking initiation. Table 4 illustrates how close together the values are for uniform and total elongation of aluminum alloys.

Table 4Another formability measure is plastic anisotropy (resistance to thinning), or r-value, often referred to as the Lankford coefficient. Aluminum alloys may have r values as low as 0.3, depending on the rolling direction, alloy and temper. The grades investigated here have r-values less than 1, indicating that they will thin more quickly than their width reduction. A draw-quality steel, on the other hand, has an r value of 2.3. Per Table 4, at the same extension level, DX55 may thin only half that of AA5754-H111. Thus, during deep drawing, the aluminum grade will exhibit excessive thinning well earlier than with steel.

Special Care in Testing and Simulation

5xxx-series aluminum alloys may exhibit nonhomogeneous behavior such as yield-point elongation and serrated flow, both visible in Fig. 1. During material-characterization tests, special care must be taken for determining r-value. The latest revision of ISO 10113—Determination of plastic strain ratio—explains how the width measurement should be taken for such materials. 

When simulating sheet metal forming, successful results rely on accurate material cards. Lacking reliable experimental data, someone might possibly create a material card with r-values entered as 1-1-1, for rolling, transverse and diagonal directions. This may work fine with some steels, as their r-values typically are higher than 1, so the thinning behavior would be overestimated but the process design would be safe. 

However, aluminum grades typically have r-values lower than 1, so assuming an r-value of 1 would underestimate the thinning. In addition, it is well known that the typical mathematical model used to describe anisotropic yield, the Hill 1948 yield criterion, does not perform well for r-values below 1. Also, recent studies in Europe show that the Vegter 2017 mechanical test for predicting advanced yield criteria may not work well with aluminum alloys. The yield surface should be selected as BBC 2005 or Barlat 1989. 
Lastly, for forming-limit-curve estimation, the only known method for aluminum alloys is the Arcelor V9 aluminum macro, available in some commercial software. Selection of Keeler or Abspoel macros is not recommended for aluminum.

New Nomenclature

Aluminum alloys still are most commonly designated using a four-digit numbering system, sometimes followed by a letter (e.g., 6110A). Temper designations are then added, consisting of a letter and optional numbers (e.g., F, H39, T6). However, in the 2000s we saw some automotive aluminum alloys become named based on their initial yield strength—Ac120 and Ac170 for example.

More recently, aluminum suppliers and automotive OEMs have introduced new naming conventions through proprietary or collaborative standards. Examples include Al5-STD, Al5-IIC, Al6-OUT, Al6-DR and Al7-UHS. In these designations, the number represents the alloy family (5xxx, 6xxx or 7xxx), while the letter codes may correspond to:

  • STD–Standard
  • IIC–Improved intergranular corrosion
  • OUT–Outer panel
  • DR–Dent-resistant
  • UHS–Ultra-high strength

It is essential to specify which standard these names refer to, as interpretations may vary between sources. Additionally, depending on the standard, the temper designation still must be included. For example, Al5-IIC-H111 represents a specific alloy and condition within this new naming framework. MF

Industry-Related Terms: Alloys, Drawing, Form, Forming, Model, Revision, Springback, Surface, Temper Designation, Tensile Strength, Wrought, Forming, Deep Drawing, Forming
View Glossary of Metalforming Terms

Technologies: Materials

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