5052 aluminum sheet strength
Looking at its specific mechanical properties 000 psi, with a yield point of 28, aluminum 5052 ( H32) has a tensile strength of 33 000 psi. 6 mm it has an elongation at break of 12% a modulus of elasticity of 10 200 ksi. 5 percent magnesium. Aluminum 5052 is one of the higher strength non- heat treatable alloys ( Annealed it is stronger than 11). Ultimate Tensile Strength psi: 28, psi: 33, 000: Yield Strength 000: Brinell Hardness: 60: Chemistry: Aluminum ( Al).
It is one of the highest strength alloys of the non- heat treatable grades. 25% chromium alloy commonly available in flat rolled coil sheet plate from a wide range of producing mills. 5052- H32 contains 2. 25% max: 5052- H32 Sheet / Plate; 5052- H32 Sheet DFARS; Value Packs - Sample Sheet. 5052- H32 Aluminum: Minimum Properties. 4% max: Magnesium ( Mg) 2.
5052 aluminum sheet strength. It has a listed Brinell hardness of 60. The 5052 aluminum sheet is highly resistant to corrosion. Both have a smooth semi- shiny finish is popular for many sheet applications. 1% max: Silicon ( Si) 0. 5052 aluminum sheet of Haomei Alu is certificated to ASTM B209 and it can be cut to size at customers' need. Aluminium Alloy Data Sheet 5052 Revised October Page 1 of 3. Aluminium Development Council of Australia PRODUCT DATA SHEET Aluminium 5052 UNS A95052 Aluminium Alloys Aluminium alloy 5052 contains nominally 2. aluminum 6061 Aluminum Sheet is ideal for. aluminum Atlas Aluminium datasheet 5052 rev Oct. 5052 is far stronger than the 1100 3000 series aluminums yet forms with reasonable bend radii. 5% magnesium & 0. Aluminium Alloy Data Sheet 5052 Revised October Page 1 of 3 www. The main content is Mg, which improve the strength of 5052 aluminum sheet. Alloy 5052 has excellent characteristics with a high fatigue strength it is used for structures which are subject to excessive vibrations. 5052 aluminum sheet strength. It has very good corrosion resistance to seawater the marine industrial atmosphere. It has good workability high fatigue strength, , very good corrosion resistance, good weldability, medium static strength especially in marine atmospheres. au Alloy 5052 is a non- heat- treatable 2½% magnesium, 0. It’ s widely sheet used because of its formability and durability. If you have any questions good suggestions on our products , , send to us, if you want to know more information about our products, please write them , site we will contact you within one business day. It is one of the highest strength. 5052 Aluminum alloy has good workability a high fatigue strength is very good for welding. 8% : Manganese ( Mn) 0. aluminum 5052 strength.
It has high fatigue and medium static strength. Properties of 5052 Aluminum Sheet. 25 percent chromium and 2. a wide range of producing mills. 6061 Aluminum Sheet is heat sheet treatable is easy to weld , resists cracking due to stress, machine but limited on formability.
At a thickness of 1. Typical applications include aircraft fuel/ oil lines , other transportation areas, wire, appliances , sheet metal work, fuel tanks, lighting rivets. 3003 Aluminum Sheet & 5052 Aluminum Sheet 3003 aluminum sheet which makes 30 sheet aluminum sheet a popular , 5052 aluminum sheet provide excellent weldability , formability, with good corrosion resistance economical choice. 6061- T651 Aluminum Sheet - ( ASTM B209 QQ- A- 250/ 11) Offers a combination of increased strength, , corrosion resistance machinability making it the most widely used aluminum grade. When magnesium is used as the major alloying element , in combination with manganese the result is a moderate to high strength non- heat treatable aluminum alloy.
It is an alloy that contains 0.
Aluminum Sheet - 3003, 5052, 6061. 3003- H14 Aluminum Sheet - ( ASTM B209,. Offers a combination of increased strength, corrosion resistance, and machinability making it the most widely used aluminum grade. 6061 Aluminum Sheet is heat treatable, resists cracking due to stress,. 5052 Aluminum Sheet.
5052 aluminum sheet strength
5052 is alloyed with 2. Tensile strength range is 31 to 44 KSI.