Alloy 321 shows good general corrosion resistance that is similar to 304. It was created for use in the chromium carbide precipitation scope by 1800–1500°F (427–816°C) where un-stabilized alloys for example 304 are subject to intergranular attack. The alloy can be utilized in most diluted organic acids at moderate temperatures and in pure phosphoric acid at lower temperatures and up to 10% diluted solutions at high temperatures. Alloy 321 opposes polythionic acid stress corrosion cracking in hydrocarbon service. It can also be used in chloride or fluoride free caustic solutions at moderate temperatures. Alloy 321 does not perform well in chloride solutions, even in small concentrations, or in sulfuric acid service.
Machining304 stainless are not tougher than 321 stainless, this material will produce the same tough stringy chips. To work harden; slow speeds and heavy feeds will minimize this alloy’s tendency.
Welding321 Stainless steels is promptly welded by all common technique, including submerged arc. Suitable weld fillers are most frequently specified as AWS E/ER 347 or E/ER 321. This alloy is mostly considered to have comparable weldability to 304 and 304L stainless with the prime difference being the titanium addition which removes or prevents carbide precipitation during welding.
Hot WorkingWorking temperatures of 2100-2300 F (1149-1260 C) are suggested for forging, upsetting and other hot work process. Don’t work this alloy at temperatures beneath 1700 F (927 C). Material must be water quenched or completely annealed after working to reattain maximum corrosion resistance.
Cold WorkingIn spite of the fact that this material requires higher initial forces than 304 stainless steels, it is slightly tough and ductile and can be easily stamped, blanked, spun and drawn.
AnnealingAnnealing at 1800-2000 F (928-1093 C) air cool. This process will result in maximum ductility. For maximum corrosion resistance, see the note on settled anneal under corrosion.
HardeningThis alloy doesn’t harden by heat treating. High properties may only be obtained through cold reduction.
Chemical Composition %Grade | C | N | Si | P | S | Cr | Mn | Ni | Fe | Ti |
321 | 0.08 max | 0.10 max | 1.0 max | 0.045 max | 0.03 max | 17.0 - 19.0 | 2.0 max | 9.0 - 12.0 | Remainder | 5x(C+N)-0.70 |
321H | 0.04 - 0.10 | 0.10 max | 1.0 max | 0.045 max | 0.03 max | 17.0 - 19.0 | 2.0 max | 9.0 - 12.0 | Remainder | 4x(C+N)-0.70 |
Tensile Strength (ksi) | 0.2% Yield Strength (ksi) | Elongation% in 2 inches |
75 | 30 | 40 |
Units | Temperature in °C | |
Density | 7.92 g/cm³ | Room |
Specific Heat | 0.12 Kcal/kg.C | 22° |
Melting Range | 1371 - 1400 °C | - |
Modulus of Elasticity | 193 KN/mm² | 20° |
Electrical Resistivity | 72 µΩ.cm | Room |
Coefficient of Expansion | 16.6 µm/m °C | 20 - 100° |
Thermal Conductivity | 16.0 W/m -°K | 20° |
Pipe / Tube (SMLS) | Sheet / Plate | Bar | Forging | Fitting |
A 213, A 249 | A 167, A 240 | A 276 | A 182 | A403 |
Manufacturing |
Refractory Anchors |
Fasteners |
Custom Machining |
Custom Fabrication |
Piping / Spools |
Stamped Parts |
B/W Fittings |
S/W Fittings |
Flanges |
Compression Fittings |
Raw Materials |
Pipes |
Tubes |
Bars |
Sheets |
Plates |