Best practices for V-notched shear testing of composites

In my October 2015 column, I wrote an overview of the widely used V-notched shear test methods for composite materials. In this column, we focus on some additional best practices when performing V-notched shear testing of fiber-reinforced composites.

In my October 2015 column, I wrote an overview of the widely used V-notched shear test methods for composite materials:

• The V-notched beam “Iosipescu” shear test, ASTM D 5379.1

• The V-notched rail shear test, ASTM D 7078.2

 • The V-notched combined loading shear test.

There are important differences among these three test
 methods. These include the specimen size and the loading method 
(edge loading, face loading or both). However, all three methods 
feature the same V-notched test section with opposing 90° notches machined to a depth that is 20-23% of the full specimen width (Fig.
 1). is reduced cross-sectional area between the notches
 produces the highest shear stresses and, therefore, specimen 
failure in the central test section.

Although the increase in shear stress due to the notched test section is easy to understand, the use of
 V-notches to produce a uniform shear stress state is less obvious. The presence of notches is generally associated with stress concentrations, 
and, in fact, the V-notches shown in Fig. 1 would
 produce significant stress concentrations if the 
notched specimen were axially loaded in tension
 or compression. Under shear loading, however, 
the 90° V-notches do not produce significant
 stress concentrations. They, in fact, significantly 
increase the uniformity of the shear stress distribution compared to unnotched specimens.
 Without notches, the shear stress has a parabolic
 distribution across the specimen width, ranging
 in magnitude from zero at the outer edges to a 
maximum at the horizontal midplane. The high 
uniformity achieved with V notches, coupled
 with a higher magnitude of shear stress in the
 central test section between the V-notches is highly desirable
 for accurate shear modulus and shear strength measurements 
of composites. In this column, we focus on some additional best practices when performing V-notched shear testing of fiber-reinforced composites.

Perhaps the most important consideration for V-notched
 shear testing is the choice of composite laminate used to
 measure the in-plane shear modulus, G12, and shear strength, S12. Because these quantities are known to be lamina or unidirectional laminate properties, it’s not surprising that unidirectional composite laminates are commonly used for testing. Additionally, because shear stresses act on the horizontal and vertical planes (Fig. 1), either a 0° (horizontal) or 90° (vertical) fiber orientation may be used. Therefore, in theory, the two fiber orientations should produce the same results. However, the 90° fiber orientation is rarely used because even a small stress concentration at the notch tips, or a crack produced during specimen preparation or handling, can lead to a sudden, premature failure (Fig. 2a). The use of a 0° fiber orientation is a better choice because the horizontal fiber orientation eliminates the weak vertical plane between the notches. However, the 0° fiber orientation produces a small stress concentration at the notch tips due to the significant material orthotropy — the large difference in stiffness between the horizontal (E1) and vertical (E2) directions.

These notch-tip stress concentrations, coupled with the weak horizontal planes in the specimen, can result in the formation of short horizontal cracks that form at the notch tips and produce a small load drop (Fig. 2b). Although these notch-tip cracks and the associated load drop were of concern during the development of the original V-notched beam test, they were found to not significantly affect the measured values of G12 or S12.3 Rather, the notch-tip cracks relieved the stress concentration produced in the 0° unidirectional specimens and permitted further loading until shear failure occurred in the specimen test section.

A less obvious candidate laminate for measuring the in-plane shear properties G12 and S12 is a cross-ply laminate, consisting
 of 0° and 90° plies. As shown in Fig. 1, the 0° and 90° plies are subjected to the same state of shear stress, as if they were part of a unidirectional laminate. Thus, in theory, a cross-ply laminate should produce the same result as either of the unidirectional laminates under pure shear loading.

However, there are significant advantages to using a [0/90]ns cross-ply laminate for in-plane shear testing. For starters, cross-ply specimens do not have a weak plane that exists in the unidirectional laminates. Thus, they are significantly less fragile and do not experience the premature cracking that occurs when using either the 0° or 90° unidirectional laminates. Additionally, cross-ply laminates do not have the high orthotropy ratio of the unidirectional laminates and consequently produce a more uniform distribution of shear stress and shear strain in the notched test section of the specimen, and minimal stress concentration at the notch tips. While desirable features for the accurate measurement of S12, they are even more important for measuring G12 during the initial stage of loading. The shear modulus is calculated using the formula:

Note that the average shear stress,τ12, is used in this equation, calculated as the applied shear force divided by the specimen cross-sectional area between the notches. Thus, to produce the correct value of G12, the average value of shear strain, γ12, also must be used. For strain gages to measure this average shear strain value, they must be located within regions of the specimen test section in which this average shear strain exists. In Fig. 3, this region corresponds to the white-colored regions, in which the shear strain is close to the average notch-to-notch value. For the cross-ply laminate (Fig. 3b), a suitable region of average shear strain is present in a relatively large region centered between the V-notches. For a 0° carbon/epoxy specimen (Fig. 3a), however, the shear strain in the central region of the specimen is approximately 10% lower than the average value, with this central value dependent upon the orthotropy ratio (E1/E2) of the material being tested.

Using this lower value of shear strain in the above equation will result in a calculated G12 value about 10% greater than 
the correct value, even when all other aspects of the test are performed properly. This error, produced by using conventional strain gages in the central region of the 0° unidirectional specimen, may be eliminated by using specialized shear strain gages that are of narrow rectangular shape and extend from notch tip to notch tip, allowing for the average shear strain to be obtained over the nonuniform area. However, such shear strain gages are currently available only for the smaller V-notched beam (ASTM D 5379) specimen4. Thus for measuring the in-plane shear modulus G12 and shear strength S12 of composite materials, the use of cross-ply laminates consisting of 0° and 90° plies is recommended.

References

1ASTM D 5379/D 5379 M-12, “Standard Test Method for Shear Properties of Composite Materials by the V-Notched Beam Method,” ASTM International (W. Conshohocken, PA, US), 2012 (first issued in 1993).
2ASTM D 7078/D 7078 M-12, “Standard Test Method for Shear Properties of Composite Materials by the V-Notched Rail Shear Method,” ASTM International (W. Conshohocken, PA, US), 2012 (first issued in 2005).

3D.F. Adams and E. Q. Lewis, “Experimental Strain Analysis of the losipescu Shear Test Specimen,” Experimental Mechanics, Vol. 35 No. 3, 1995, pp. 352-360.

4“Plane-Shear Measurement with Strain Gages,” Vishay Precision Group Tech Note TN-512-1, Document No. 11062, September 2010, online at www.vishaypg.com/docs/11062/tn5121tn.pdf
5D.O. Adams, J.M. Moriarty, A.M. Gallegos, and D.F. Adams, “Development and Evaluation of the V-Notched Rail Shear Test for Composite Laminates,” Federal Aviation Administration Report No. DOT/FAA/AR-03/63, September 2003, online at www.tc.faa.gov/its/worldpac/techrpt/ ar03-63.pdf 

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