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Aluminum alloys 3003
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Journal Articles
Alloy Digest (1987) 36 (11): Al-284.
Published: 01 November 1987
... AA 3003 is a wrought non-heat-treatable aluminum alloy with excellent resistance to corrosion. It is used widely in deep-drawing and forming applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear...
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AA 3003 is a wrought non-heat-treatable aluminum alloy with excellent resistance to corrosion. It is used widely in deep-drawing and forming applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-284. Producer or source: Aluminum producers.
Journal Articles
Alloy Digest (1973) 22 (12): Al-31.
Published: 01 December 1973
... ALUMINUM 3003 is a wrought non-heat-treatable aluminum alloy with excellent resistance to corrosion. It is used widely in deep-drawing and forming applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive...
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ALUMINUM 3003 is a wrought non-heat-treatable aluminum alloy with excellent resistance to corrosion. It is used widely in deep-drawing and forming applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-31. Producer or source: Various aluminum companies. Originally published September 1955, revised December 1973.
Journal Articles
Alloy Digest (2021) 70 (6): Al-477.
Published: 01 June 2021
... Atlas Steels 3003 is a non-heat-treatable, aluminum-manganese-copper alloy. It is one of the most commonly used aluminum alloys. It is selected for applications where good formability, very good resistance to corrosion, or good weldability, or all three, are required, and where more strength...
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Atlas Steels 3003 is a non-heat-treatable, aluminum-manganese-copper alloy. It is one of the most commonly used aluminum alloys. It is selected for applications where good formability, very good resistance to corrosion, or good weldability, or all three, are required, and where more strength is desired than is provided by unalloyed aluminum. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-477. Producer or source: Atlas Steels.
Journal Articles
Alloy Digest (1974) 23 (4): Al-51.
Published: 01 April 1974
... ALUMINUM 3004 is nominally an aluminum-manganese-magnesium alloy which cannot be hardened by heat treatment; however, it can be strain hardened by cold working. It has higher strength than Aluminum 3003 and good workability, weldability and resistance to corrosion. This datasheet provides...
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ALUMINUM 3004 is nominally an aluminum-manganese-magnesium alloy which cannot be hardened by heat treatment; however, it can be strain hardened by cold working. It has higher strength than Aluminum 3003 and good workability, weldability and resistance to corrosion. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-51. Producer or source: Various aluminum companies. Originally published June 1957, revised April 1974.
Journal Articles
Alloy Digest (2017) 66 (2): Al-452.
Published: 01 February 2017
... specimen, MPa (ksi) 110 (16) Yield strength, 12.7 mm (0.5 in.) diameter specimen, MPa (ksi) 41 (6) Elongation, 4D, 12.7 mm (0.5 in.) diameter specimen, % 25 Copyright © 2017, ASM International®. All rights reserved. KAISER ALLOY 3003 (High Strength Alloy) Filing Code: Al-452 Aluminum :: February 2017...
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Kaiser Alloy 3003 is a general engineering alloy produced as tubing. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, machining, and joining. Filing Code: Al-452. Producer or source: Kaiser Aluminum Corporation.
Journal Articles
Alloy Digest (2022) 71 (2): Al-485.
Published: 01 February 2022
... Austral Wright 3003 (UNS A93003) is a wrought, non-heat-treatable, aluminum-manganese-copper alloy (3xxx series). It is used in a wide variety of applications where moderate strength, good formability, and good resistance to corrosion are important. This datasheet provides information...
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Austral Wright 3003 (UNS A93003) is a wrought, non-heat-treatable, aluminum-manganese-copper alloy (3xxx series). It is used in a wide variety of applications where moderate strength, good formability, and good resistance to corrosion are important. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as heat treating, machining, and joinability. Filing Code: Al-485. Producer or source: Austral Wright Metals.
Journal Articles
Alloy Digest (2002) 51 (8): Al-380.
Published: 01 August 2002
... 4.5 6.0 Iron 0.8 max Copper 0.30 max Manganese 0.05 max Magnesium 0.05 max Zinc 0.15 max Titanium 0.20 max Beryllium 0.0008 max Others, each 0.05 max Others, total 0.15 max Aluminum bal Physical Properties: Density, kg/m3 (lb/in.3 ) 2685 (0.097) Conductivity, O temper, %IACS 42 Melting range, °C (°F...
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AlcoTec weld filler wire 4043 is a general-purpose high-silicon-containing wire for both welding and brazing. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on joining. Filing Code: AL-380. Producer or source: AlcoTec Wire Corporation.
Journal Articles
Alloy Digest (1958) 7 (3): Al-64.
Published: 01 March 1958
... 3003 (formerly 3S), the alloys heretofore most widely used for aluminum pressure vessels. For operating temperatures up to lOOoF. in pressure vessels, the maximum allowable stress in ten- sion is 7350 psi for the annealed sheet and plate. Maximum service temperature is 300°F. Its favorable low...
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ALUMINUM 5154, formerly known as Aluminum A54S, is a strong, nonheat-treatable alloy recommended for use in unfired pressure vessels. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-64. Producer or source: Aluminum Company of America.
Journal Articles
Alloy Digest (2002) 51 (9): Al-381.
Published: 01 September 2002
... properties Chemical Composition, wt Silicon 11.0 13.0 Iron 0.8 max Copper 0.30 max Manganese 0.15 max Magnesium 0.10 max Zinc 0.20 max Beryllium 0.0008 max Others, each 0.05 max Others, total 0.15 max Aluminum bal Physical Properties: Density, kg/m3 (lb/in.3 ) 2657 (0.096) Electrical conductivity, 41 O...
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AlcoTec weld filler wire 4047 is a general-purpose high silicon containing wire for both welding and brazing. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on joining. Filing Code: AL-381. Producer or source: AlcoTec Wire Corporation.
Journal Articles
Alloy Digest (1973) 22 (6): Al-39.
Published: 01 June 1973
... is of the wrought strain-hardening type, i.e., its various tempers are produced by subjecting it to definite reductions by cold working. The harder the temper the greater the strength of the alloy and the lower the elongation It has mechanical properties intermediate between those of Aluminum 1100 and 3003...
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ALUMINUM 5052 is nominally an aluminum-magnesium-chromium alloy which cannot be hardened by heat treatment; however, it can be strain hardened by cold working. It combines good workability with good fatigue strength and high corrosion resistance to the atomsphere and to salt water. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-39. Producer or source: Various aluminum companies. Originally published May 1956, revised June 1971, revised June 1973.
Journal Articles
Alloy Digest (2022) 71 (8): Al-489.
Published: 01 August 2022
... Austral Wright 5005 is a wrought, non-heat-treatable, aluminum-magnesium alloy (5xxx series) that exhibits moderate strength, good formability, and good resistance to corrosion in marine atmospheres. It is widely used for decorative and architectural applications. This datasheet provides...
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Austral Wright 5005 is a wrought, non-heat-treatable, aluminum-magnesium alloy (5xxx series) that exhibits moderate strength, good formability, and good resistance to corrosion in marine atmospheres. It is widely used for decorative and architectural applications. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-489. Producer or source: Austral Wright Metals.
Journal Articles
Alloy Digest (1979) 28 (9): Al-157.
Published: 01 September 1979
... ALUMINUM 5254 is an aluminum-magnesium-chromium wrought alloy of the non-heat-treatable type; however, it can be hardened and strengthened by cold working. It is relatively strong and has excellent resistance to general corrosion and stress-corrosion cracking. Its applications include hydrogen...
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ALUMINUM 5254 is an aluminum-magnesium-chromium wrought alloy of the non-heat-treatable type; however, it can be hardened and strengthened by cold working. It is relatively strong and has excellent resistance to general corrosion and stress-corrosion cracking. Its applications include hydrogen peroxide serivce and chemical storage vessels. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-157. Producer or source: Various aluminum companies. Originally published August 1966, revised September 1979.
Journal Articles
Alloy Digest (1978) 27 (11): Al-38.
Published: 01 November 1978
... aBoys high in magnesium, it does not have the usual dark coloration. It is well suited for anodizing applications since it exhibits less tendency toward structural streaking. After anodizing the alloy is clearer and lighter in color than either 3003 or 5052 aluminum alloys. It is particularly desirable...
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ALUMINUM 5005 is nominally an aluminum-magnesium alloy that cannot be hardened or strengthened by heat treatment; however, it can be hardened by cold working. It has excellent resistance to corrosion, excellent weldability and good brazeability. Its numerous applications include appliances, utensils and architectural components. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-38. Producer or source: Various aluminum companies. Originally published April 1956, revised April 1973, revised November 1978.
Journal Articles
Alloy Digest (1955) 4 (8): Al-30.
Published: 01 August 1955
... ALUMINUM 5357 is an aluminum-magnesium-manganese alloy of the non-heat-treatable type. Formerly known as Aluminum C57S or Aluminum K157. This datasheet provides information on composition, physical properties, hardness, tensile properties, and shear and bearing strength. It also includes...
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ALUMINUM 5357 is an aluminum-magnesium-manganese alloy of the non-heat-treatable type. Formerly known as Aluminum C57S or Aluminum K157. This datasheet provides information on composition, physical properties, hardness, tensile properties, and shear and bearing strength. It also includes information on as well as forming, machining, and joining. Filing Code: Al-30. Producer or source: Aluminum Company of America.
Journal Articles
Alloy Digest (1963) 12 (8): Al-128.
Published: 01 August 1963
... Alcan B51S is a medium strength, heat treatable aluminum structural alloy. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining...
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Alcan B51S is a medium strength, heat treatable aluminum structural alloy. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-128. Producer or source: Aluminum Company of Canada Ltd.
Journal Articles
Alloy Digest (1968) 17 (6): Al-176.
Published: 01 June 1968
... Aluminum 5557 is an aluminum alloy having good bright finishing characteristics. It has good formability and weldability. It is recommended for finishing and decorative applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties...
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Aluminum 5557 is an aluminum alloy having good bright finishing characteristics. It has good formability and weldability. It is recommended for finishing and decorative applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-176. Producer or source: Aluminum Company of America.
Journal Articles
Alloy Digest (1970) 19 (5): Al-196.
Published: 01 May 1970
... radii Heat Treatment: This alloy does not respond to any age-hardening heat treatment. It is strengthened and hardened by cold work only. Machinability: Aluminum 3105 has fait machinability rating. Its machining characteristics are similar to those of Aluminum 3003 alloy. Cutting tools should have large...
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Aluminum 3105 is a non-heat treatable aluminum alloy sheet material having excellent weldability, formability and corrosion resistance. It is recommended for appliances, trim and containers. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-196. Producer or source: Aluminum Company of America.
Journal Articles
Alloy Digest (1968) 17 (3): Al-173.
Published: 01 March 1968
... stick provides sufficient lubrication and prevents gumming the wheel. Workability: Readily formed. In rhe annealed state the forming quality is similar to aluminum 1100-O and 3003-O alloys; in the heat treated and heat treated plus aged tempers it forms more nearly like aluminum 1100 in rhe hard temper...
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Aluminum 6563 is an aluminum extrusion alloy recommended for trim applications, combining medium strength and formability with good finishing characteristics. It responds to an age-hardening heat treatment. Alloy 6563 is a modification of alloy 6063 with improved finishing characteristics and somewhat lower mechanical properties. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Al-173. Producer or source: Aluminum Company of America.
Journal Articles
Alloy Digest (1958) 7 (7): Al-67.
Published: 01 July 1958
... ALUMINUM 6151, formerly A51S Alloy, is an aluminum forging alloy combining good forgeability, strength, and resistance to corrosion. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties...
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ALUMINUM 6151, formerly A51S Alloy, is an aluminum forging alloy combining good forgeability, strength, and resistance to corrosion. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Al-67. Producer or source: Aluminum Company of America.
Journal Articles
Alloy Digest (1980) 29 (8): Al-178.
Published: 01 August 1980
... ALUMINUM 5657 is an aluminum-base, wrought, non-heat-treatable alloy of high purity and bright appearance. It has high resistance to general corrosion and to stress-corrosion cracking. It is used widely in the anodized condition for automotive and appliance trim. This datasheet provides...
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ALUMINUM 5657 is an aluminum-base, wrought, non-heat-treatable alloy of high purity and bright appearance. It has high resistance to general corrosion and to stress-corrosion cracking. It is used widely in the anodized condition for automotive and appliance trim. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-178. Producer or source: Various aluminum companies. Originally published August 1968, revised August 1980.
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