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WMT&R performs
tensile tests up to 1,000,000 lbs capacity at ambient
temperature. We also perform
tests at temperatures ranging from
-423°F to 2200°F in accordance with
customer unique specifications as well as the following international
and industry standards:
ASTM E 8, Standard Test Methods for Tension Testing of Metallic
Materials,
ASTM E 21, Standard Test Methods for Elevated
Temperature Tension Tests of Metallic Materials,
Mil-STD-1312-18 superseded by NASM1312-18, Standard
Practice, National Aerospace Standard, Fastener Test Methods; Method 18,
Elevated Temperature Tensile Strength,
Mil-STD-1312-8 superseded by, NASM1312-8, Standard Practice,
National Aerospace Standard, Fastener Test Methods, Method 8, Tensile
Strength,
ASTM A 370, Standard Test Methods and Definitions for
Mechanical Testing of Steel Products, Sections 5-13 Tension,
ASTM D 638, Standard
Test Method for Tensile Properties of Plastics,
ASTM F 606
/ F 606 M, Standard Test Methods for Determining the Mechanical
Properties of Externally and Internally Threaded Fasteners, Washers,
Direct Tension Indicators, and Rivets,
ASTM D 3039/D 3039M,
Standard Test Method for Tensile Properties of Polymer Matrix Composite
Materials.
In
a Tensile Test an axial pull is exerted upon
the material in accordance with agreed upon standards, and the results
measured with scientifically accurate methods. Ultimate Tensile
Strength, Yield Strength, True Stress and Strain, Engineering Stress and
Strain, the Elastic Modulus, the the Fracture Stress, the Modulus of
Toughness, and the Modulus of Resilience, may all be determined by this
test
Many properties of a material may be
determined by use of the Tensile Test.
Ultimate Tensile Strength is determined by
dividing the highest load experienced by the specimen before
rupture by the original cross section of the test specimen.
Yield Strength is determined by the amount of stress that is
required to begin plastic deformation of the test specimen.
The Elastic Modulus or Young's
Modulus is determined by the ratio of
stress to strain below the elastic limit. The Modulus of Elasticity
measures the stiffness of a material but it only applies to the portion
of the test where the ratio of stress to strain is constant. On an x y
axis graph of the Tensile Test this portion of the test would be
represented by the straight line portion of the graph prior to the
beginning of the curve. At this point in the test, if the load were to
be removed, the test specimen would return to its original condition.
After this point in the test, plastic deformation begins to occur, and
the test specimen will not return to its original proportions upon
relaxation of the load.
The Offset Method for determining Yield Strength
is used when the material being tested does not show an easily identifiable
departure point from the linear elastic region on the graph. Many metals and
most plastics fall into this category. An offset is specified as a % of
strain. A line is drawn from the offset with the same slope as the Modulus
of Elasticity. The stress value at the intersection of the offset line with
the line of the linear elastic region is then used for the Yield Strength by
Offset Method.
Modulus of Toughness is
determined in the Tensile Test by calculating the total area under the
stress/strain curve to the point of failure.
Modulus of Resilience
is the energy that can be absorbed per unit volume
without causing permanent distortion. And may be calculated by
integrating the stress/strain curve from zero to the elastic limit and
then dividing by the original volume.
Fracture stress
is the load at fracture divided by the cross sectional area at fracture.
Engineering Stress and
Strain is the ratio of the applied
load to the undeformed cross-sectional area, while, True Stress and
Strain is the ratio of the applied force to the instantaneous
cross-sectional area. True Stress and Strain calculates for the reduced
area of the test specimen as plastic deformation occurs. for most
applications involving small strain rates (less than 5%) Engineering
Stress and Strain are accurate enough. For larger strain rates, the
more involved calculations to arrive at True Stress and Strain become
necessary. For a more in depth treatment of this subject visit
Key To Steel.
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