Aluminum
Aluminum 5086
Aging Procedure
Not applicable to this alloy.
Annealing Procedure
Anneal at 650 F for long enough to insure thorough heating. Air cool.
Applications
Commonly used in the manufacture of unfired, welded pressure vessels, marine, auto aircraft cryogenics, drilling rigs, tanks, TV towers, transportation equipment, and in missile components.
Cold Workability
Excellent cold working characteristics in the O temper and somewhat less good in H36 and H38 tempers.
Forgeability
No specific data as to hot working range. However the alloy is forgeable.
Formability
Forming characteristics are best with the alloy in the O temper -- less good in the H36 or H38 tempers.
Hardening Procedure
Hardens by cold working only.
Heat Treatability
The alloy is non-heat treatable.
Hot Workability
No data in regard to hot forming. Cold forming characteristics are excellent and usually would not necessitate hot working.
Machinability
Machinability in the strain hardened tempers (H34, H36, H38) is relatively good. In the annealed (O temper) machining is difficult, but still can be accomplished. Use of lubricants is advised.
Other Mechanical Properties
Shear strength for O temper is 23 ksi, for H34 it is 27 ksi
Other Physical Properties
Electrical conductivity 30% of copper.
Principle Design Features
This is a high strength structural alloy. It is not heat treatable.
Tempering Procedure
Not applicable.
Weldability
This alloy is readily weldable by conventional methods. Use of electric arc welding in particular produces excellent results.
Known Forms
Angle
Channel
Coil
Disc
Flat Bar
Foil
Hollow Bar
Pipe
Plate
Rectangle Tube
Ring
Rod
Round Bar
Round Tube
Sheet
Square Bar
Square Tube
Strip
Tee
Treadplate
Additional Data
Specifications
B209,B210,B221,B241,B313,B345,B361,B547,B548,C-26094,S-24149/2,A-200/5,A-250/7,WW-T-700/5,J454,A95086Chemical Elements
| Aluminum | Balance |
| Chromium | 0.05 - 0.25 |
| Copper | 0.1 max |
| Iron | 0.5 max |
| Magnesium | 3.5 - 4.5 |
| Manganese | 0.2 - 0.7 |
| Remainder Each | 0.05 max |
| Remainder Total | 0.15 max |
| Silicon | 0.4 max |
| Titanium | 0.15 max |
| Zinc | 0.25 max |
Physical Properties
Density: 0.096lb/in³
Melting Point: 1090°F
Specific Gravity: 2.66
Mechanical Properties
Modulus of Elasticity – Tension: 10.3MSI
Mechanical Test Data
| Form | Sheet |
| Condition | H112 |
| Temperature | 68°F |
| Elongation | 14% |
| Tensile Strength | 39 KSI |
| Yield Strength | 19 KSI |
| Form | Sheet |
| Condition | H116 |
| Temperature | 68°F |
| Elongation | 12% |
| Tensile Strength | 42 KSI |
| Yield Strength | 30 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | 68°F |
| Elongation | 12% |
| Tensile Strength | 42 KSI |
| Yield Strength | 30 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | 68°F |
| Elongation | 10% |
| Tensile Strength | 47 KSI |
| Yield Strength | 37 KSI |