General
Properties
Alloys 304 (S30400), 304L (S30403), and 304H (S30409)
stainless steels are variations of the 18 percent
chromium – 8 percent nickel austenitic alloy,
the most familiar and most frequently used alloy
in the stainless steel family. These alloys may
be considered for a wide variety of applications
where one or more of the following properties
are important:
- Resistance to corrosion
- Prevention of product contamination
- Resistance to oxidation
- Ease of fabrication
- Excellent formability
- Beauty of appearance
- Ease of cleaning
- High strength with low weight
- Good strength and toughness at
cryogenic temperatures
- Ready availability of a wide
range of product forms
Each alloy represents an excellent
combination of corrosion resistance and fabricability.
This combination of properties is the reason for
the extensive use of these alloys which represent
nearly one half of the total U.S. stainless steel
production. The 18-8 stainless steels, principally
Alloys 304, 304L, and 304H, are available in a
wide range of product forms including sheet, strip,
and plate. The alloys are covered by a variety
of specifications and codes relating to, or regulating,
construction or use of equipment manufactured
from these alloys for specific conditions. Food
and beverage, sanitary, cryogenic, and pressure-containing
applications are examples.
Alloy 304 is the standard alloy
since AOD technology has made lower carbon levels
more easily attainable and economical. Alloy 304L
is used for welded products which might be exposed
to conditions which could cause intergranular
corrosion in service.
Alloy 304H is a modification of
Alloy 304 in which the carbon content is controlled
to a range of 0.04-0.10 to provide improved high
temperature strength to parts exposed to temperatures
above 800°F.
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Chemical
Composition
Chemistries per ASTM A240 and ASME SA-240:
| Element |
Percentage
by Weight
Maximum Unless Range is Specified |
| |
304 |
304L |
304H |
| Carbon |
0.08 |
0.030 |
0.04-0.01 |
| Manganese |
2.00 |
2.00 |
2.00 |
| Phosphorus |
0.045 |
0.045 |
0.045 |
| Sulfur |
0.030 |
0.030 |
0.030 |
| Silicon |
0.75 |
0.75 |
0.75 |
| Chromium |
18.00
20.00 |
18.00
20.00 |
18.00
20.00 |
| Nickel |
8.0
10.50 |
8.0
12.00 |
8.0
10.5 |
| Nitrogen |
0.10 |
0.10 |
0.10 |
Data are typical and should not
be construed as maximum or minimum values for
specification or for final design. Data on any
particular piece of material may vary from those
shown herein.
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Resistance
to Corrosion
General Corrosion
The Alloys 304, 304L, and 304H austenitic stainless
steels provide useful resistance to corrosion
on a wide range of moderately oxidizing to moderately
reducing environments. The alloys are used widely
in equipment and utensils for processing and handling
of food, beverages, and dairy products. Heat exchangers,
piping, tanks, and other process equipment in
contact with fresh water also utilize these alloys.
The 18 to 19 percent of chromium
which these alloys contain provides resistance
to oxidizing environments such as dilute nitric
acid, as illustrated by data for Alloy 304 below.
| % Nitric Acid |
Temperature
°F (°C) |
Corrosion Rate
Mils/Yr (mm/a) |
| 10 |
300 (149) |
5.0 (0.13) |
| 20 |
300 (149) |
10.1 (0.25) |
| 30 |
300 (149) |
17.0 (0.43) |
Alloys 304, 304L, and 304H are also
resistant to moderately aggressive organic acids
such as acetic and reducing acids such as phosphoric.
The 9 to 11 percent of nickel contained by these
18-8 alloys assists in providing resistance to
moderately reducing environments. The more highly
reducing environments such as boiling dilute hydrochloric
and sulfuric acids are shown to be too aggressive
for these materials. Boiling 50 percent caustic
is likewise too aggressive.
In some cases, the low carbon Alloy
304L may show a lower corrosion rate than the
higher carbon Alloy 304. The data for formic acid,
sulfamic acid, and sodium hydroxide illustrate
this. Otherwise, the Alloys 304, 304L, and 304H
may be considered to perform equally in most corrosive
environments. A notable exception is in environments
sufficiently corrosive to cause intergranular
corrosion of welds and heat-affected zones on
susceptible alloys. The Alloy 304L is preferred
for use in such media in the welded condition
since the low carbon level enhances resistance
to intergranular corrosion.
Intergranular Corrosion
Exposure of the 18-8 austenitic stainless steels
to temperatures in the 800°F to 1500°F
(427°C to 816°C) range may cause precipitation
of chromium carbides in grain boundaries. Such
steels are "sensitized" and subject
to intergranular corrosion when exposed to aggressive
environments. The carbon content of Alloy 304
may allow sensitization to occur from thermal
conditions experienced by autogenous welds and
heat-affected zones of welds. For this reason,
the low carbon Alloy 304L is preferred for applications
in which the material is put into service in the
as-welded condition. Low carbon content extends
the time necessary to precipitate a harmful level
of chromium carbides but does not eliminate the
precipitation reaction for material held for long
times in the precipitation temperature range.
| Intergranular
Corrosion Tests |
ASTM
A262
Evaluation
Test |
Corrosion
Rate, Mils/Yr (mm/a) |
| 304 |
304L |
Practice
E Base Metal Welded |
No Fissures on
Bend
Some Fissures on Weld
(unacceptable) |
No Fissures
No Fissures |
Practice
A Base Metal Welded |
Step Structure
Ditched
(unacceptable) |
Step Structure
Step Structure |
Stress Corrosion Cracking
The Alloys 304, 304L, and 304H are the most susceptible
of the austenitic stainless steels to stress corrosion
cracking (SCC) in halides because of their relatively
low nickel content. Conditions which cause SCC
are: (1) presence of halide ions (generally chloride),
(2) residual tensile stresses, and (3) temperatures
in excess of about 120°F (49°C). Stresses
may result from cold deformation of the alloy
during forming or by roller expanding tubes into
tube sheets or by welding operations which produce
stresses from the thermal cycles used. Stress
levels may be reduced by annealing or stress relieving
heat treatments following cold deformation, thereby
reducing sensitivity to halide SCC. The low carbon
Alloy 304L material is the better choice for service
in the stress-relieved condition in environments
which might cause intergranular corrosion.
| Halide (Chloride
Stress Corrosion Tests) |
| Test |
U-Bend
(Highly Stressed) Samples |
| 304 |
33%
Lithium
Chloride, Boiling |
Base
Metal
Welded |
Cracked,
14 to 96 hours
Cracked, 18 to 90 hours |
26%
Sodium
Chloride, Boiling |
Base
Metal
Welded |
Cracked,
142 to 1004 hours
Cracked, 300 to 500 hours |
40%
Calcium
Chloride, Boiling |
Base
Metal |
Cracked,
144 hours
-- |
| Ambient
Temperature Seacoast Exposure |
Base
Metal
Welded |
No
Cracking
No Cracking |
Pitting/Crevice Corrosion
The 18-8 alloys have been used very successfully
in fresh waters containing low levels of chloride
ion. Generally, 100 ppm chloride is considered
to be the limit for the 18-8 alloys, particularly
if crevices are present. Higher levels of chloride
might cause crevice corrosion and pitting. For
the more severe conditions of higher chloride
levels, lower pH, and/or higher temperatures,
alloys with higher molybdenum content such as
Alloy 316 should be considered. The 18-8 alloys
are not recommended for exposure to marine environments.
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Physical
Properties
Density:
0.285 lb/in3 (7.90 g/cm3)
Modulus of Elasticity in Tension:
29 x 106 psi (200 GPa)
Linear Coefficient of Thermal
Expansion:
| Temperature
Range |
Coefficients |
| °F |
°C |
in/in/°F |
cm/cm/°C |
| 68-212 |
20-100 |
9.2 x 10-6 |
16.6 x 10-6 |
| 18 - 1600 |
20 - 870 |
11.0 x 10-6 |
19.8 x 10-6 |
Thermal Conductivity:
| Temperature
Range |
Btu/hr/ft/°F |
W/m/K |
| °F |
°C |
| 212 |
100 |
9.4 |
16.3 |
| 932 |
500 |
12.4 |
21.4 |
The overall heat transfer coefficient
of metals is determined by factors in addition
to the thermal conductivity of the metal. The
ability of the 18-8 stainless grades to maintain
clean surfaces often allows better heat transfer
than other metals having higher thermal conductivity.
Specific Heat:
| °F |
°C |
Btu/lb/°F |
J/kg/K |
| 32-212 |
0-100 |
0.12 |
500 |
Magnetic Permeability:
The 18-8 alloys are generally non-magnetic in
the annealed condition with magnetic permeability
values typically less than 1.02 at 200H. Permeability
values will vary with composition and will increase
with cold work.
| Percent
Cold Work |
Magnetic
Permeability |
| 304 |
304L |
| 0 |
1.005 |
1.015 |
| 10 |
1.009 |
1.064 |
| 30 |
1.163 |
3.235 |
| 50 |
2.291 |
8.480 |
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Mechanical
Properties
Room Temperature Mechanical Properties
Minimum mechanical properties for annealed Alloys
304 and 304L austenitic stainless steel plate
as required by ASTM specifications A240 and ASME
specification SA-240 are shown below.
| Property |
Minimum
Mechanical Properties
Required by ASTM A240 & ASME SA-240 |
| 304 |
304L |
304H |
0.2%
Offset
Yield
Strength, psi MPa |
30,000
205 |
25,000
170 |
30,000
205 |
Ultimate
Tensile
Strength, psi MPa |
75,000
515 |
70,000
485 |
75,000
515 |
Percent
Elongation in
2 in. or 51 mm |
40.0 |
40.0 |
40.0 |
Hardness,
Max., Brinell RB |
201
92 |
201
92 |
201
92 |
Low and Elevated Temperature
Properties
Typical short time tensile property data for low
and elevated temperatures are shown below. At
temperatures of 1000°F (538°C) or higher,
creep and stress rupture become considerations.
Typical creep and stress rupture data are also
shown below.
Test
Temperature |
0.2% Yield
Strength |
Tensile
Strength |
Elongation |
| °F |
°C |
psi |
(MPa) |
psi |
(MPa) |
Percent in
2" or
51mm |
| -423 |
-253 |
100,000 |
690 |
250,000 |
1725 |
25 |
| -320 |
-196 |
70,000 |
485 |
230,000 |
1585 |
35 |
| -100 |
-79 |
50,000 |
354 |
150,000 |
1035 |
50 |
| 70 |
21 |
35,000 |
240 |
90,000 |
620 |
60 |
| 400 |
205 |
23,000 |
160 |
70,000 |
485 |
50 |
| 800 |
427 |
19,000 |
130 |
66,000 |
455 |
43 |
| 1200 |
650 |
15,500 |
105 |
48,000 |
330 |
34 |
| 1500 |
815 |
13,000 |
90 |
23,000 |
160 |
46 |
Impact Resistance
The annealed austenitic stainless steels maintain
high impact resistance even at cryogenic temperatures,
a property which, in combination with their low
temperature strength and fabricability, has led
to their use in handling liquified natural gas
and other cryogenic environments. Typical Charpy
V-notch impact data are shown below.
| Temperature |
Charpy V-Notch Energy
Absorbed |
| °F |
°C |
Foot - pounds |
Joules |
| 75 |
23 |
150 |
200 |
| -320 |
-196 |
85 |
115 |
| -425 |
-254 |
85 |
115 |
Fatigue Strength
The fatigue strength or endurance limit is the
maximum stress below which material is unlikely
to fail in 10 million cycles in air environment.
The fatigue strength for austenitic stainless
steels, as a group, is typically about 35 percent
of the tensile strength. Substantial variability
in service results is experienced since additional
variables influence fatigue strength. As examples
– increased smoothness of surface improves
strength, increased corrosivity of service environment
decreases strength.
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Welding
The austenitic stainless steels are considered
to be the most weldable of the high-alloy steels
and can be welded by all fusion and resistance
welding processes. The Alloys 304 and 304L are
typical of the austenitic stainless steels.
Two important considerations in
producing weld joints in the austenitic stainless
steels are: 1) preservation of corrosion resistance,
and 2) avoidance of cracking.
A temperature gradient is produced
in the material being welded which ranges from
above the melting temperature in the molten pool
to ambient temperature at some distance from the
weld. The higher the carbon level of the material
being welded, the greater the likelihood that
the welding thermal cycle will result in the chromium
carbide precipitation which is detrimental to
corrosion resistance. To provide material at the
best level of corrosion resistance, low carbon
material (Alloy 304L) should be used for material
put in service in the welded condition. Alternately,
full annealing dissolves the chromium carbide
and restores a high level of corrosion resistance
to the standard carbon content materials.
Weld metal with a fully austenitic
structure is more susceptible to cracking during
the welding operation. For this reason, Alloys
304 and 304L are designed to resolidify with a
small amount of ferrite to minimize cracking susceptibility.
Alloy 309 (23% Cr – 13.5%
Ni) or nickel-base filler metals are used in joining
the 18-8 austenitic alloys to carbon steel.
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Heat
Treatment
The austenitic stainless steels are heat treated
to remove the effects of cold forming or to dissolve
precipitated chromium carbides. The surest heat
treatment to accomplish both requirements is the
solution anneal which is conducted in the 1850°F
to 2050°F range (1010°C to 1121°C).
Cooling from the anneal temperature should be
at sufficiently high rates through 1500-800°F
(816°C - 427°C) to avoid reprecipitation
of chromium carbides.
These materials cannot be hardened
by heat treatment.
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Cleaning
Despite their corrosion resistance, stainless
steels need care in fabrication and use to maintain
their surface appearance even under normal conditions
of service.
In welding, inert gas processes
are used. Scale or slag that forms from welding
processes is removed with a stainless steel wire
brush. Normal carbon steel wire brushes will leave
carbon steel particles in the surface which will
eventually produce surface rusting. For more severe
applications, welded areas should be treated with
a descaling solution such as a mixture of nitric
and hydrofluoric acids, and these should be subsequently
washed off.
For material exposed inland, light
industrial, or milder service, minimum maintenance
is required. Only sheltered areas need occasional
washing with a stream of pressurized water. In
heavy industrial areas, frequent washing is advisable
to remove dirt deposits which might eventually
cause corrosion and impair the surface appearance
of the stainless steel.
Stubborn spots and deposits like
burned-on food can be removed by scrubbing with
a non-abrasive cleaner and fiber brush, a sponge,
or pad of stainless steel wool. The stainless
steel wool will leave a permanent mark on smooth
stainless steel surfaces.
Many of these uses of stainless
steel involve cleaning or sterilizing on a regular
basis. Equipment is cleaned with specially designed
caustic soda, organic solvent, or acid solutions
such as phosphoric or sulfamic acid (strongly
reducing acids such as hydrofluoric or hydrochloric
may be harmful to these stainless steels).
Cleaning solutions need to be drained
and stainless steel surfaces rinsed thoroughly
with fresh water.
Design can aid cleanability. Equipment
with rounded corners, fillets, and absence of
crevices facilitates cleaning as do smooth ground
welds and polished surfaces.
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