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Mam Tor road destroyed by subsidence and shear, near Castleton, Derbyshire.

In engineering, shear strength is the strength of a material or component against the type of yield or structural failure when the material or component fails in shear. A shear load is a force that tends to produce a sliding failure on a material along a plane that is parallel to the direction of the force. When a paper is cut with scissors, the paper fails in shear.

In structural and mechanical engineering, the shear strength of a component is important for designing the dimensions and materials to be used for the manufacture or construction of the component (e.g. beams, plates, or bolts). In a reinforced concrete beam, the main purpose of reinforcing bar (rebar) stirrups is to increase the shear strength.

Equations

For shear stress $\tau$ applies

\tau ={\frac {\sigma _{1}-\sigma _{3}}{2}},

where

\sigma _{1}

is major principal stress and

\sigma _{3}

is minor principal stress.

In general: ductile materials (e.g. aluminum) fail in shear, whereas brittle materials (e.g. cast iron) fail in tension (see: Tensile strength).

To calculate:

Given total force at failure (F) and the force-resisting area (e.g. the cross-section of a bolt loaded in shear), ultimate shear strength ( $\tau$ ) is:

\tau ={\frac {F}{A}}={\frac {F}{\pi r_{\text{bolt}}^{2}}}={\frac {4F}{\pi d_{\text{bolt}}^{2}}}

For average shear stress

$\tau _{\text{avg}}={\frac {V}{A}}$

where

\tau _{\text{avg}}

is the average shear stress,

V

is the shear force applied to each section of the part, and

A

is the area of the section.^[1]

Average shear stress can also be defined as the total force of $V$ as

V=\int \tau dA

This is only the average stress, actual stress distribution is not uniform. In real world applications, this equation only gives an approximation and the maximum shear stress would be higher. Stress is not often equally distributed across a part so the shear strength would need to be higher to account for the estimate.^[2]

Comparison

As a very rough guide relating tensile, yield, and shear strengths:^[3]

Material	Ultimate Strength Relationship	Yield Strength Relationship
Steels	USS = approx. 0.75*UTS	SYS = approx. 0.58*TYS
Ductile Iron	USS = approx. 0.9*UTS	SYS = approx. 0.75*TYS .
Malleable Iron	USS = approx. 1.0*UTS
Wrought Iron	USS = approx. 0.83*UTS
Cast Iron	USS = approx. 1.3*UTS
Aluminums	USS = approx. 0.65*UTS	SYS = approx. 0.55*TYS

USS: Ultimate Shear Strength, UTS: Ultimate Tensile Strength, SYS: Shear Yield Stress, TYS: Tensile Yield Stress

There are no published standard values for shear strength like with tensile and yield strength. Instead, it is common for it to be estimated as 60% of the ultimate tensile strength. Shear strength can be measured by a torsion test where it is equal to their torsional strength.^[4]^[5]

Material	Ultimate stress (Ksi)	Ultimate stress (MPa)
Fiberglass/epoxy (23 ^o C)^[6]	7.82	53.9

When values measured from physical samples are desired, a number of testing standards are available, covering different material categories and testing conditions. In the US, ASTM standards for measuring shear strength include ASTM B769, B831, D732, D4255, D5379, and D7078. Internationally, ISO testing standards for shear strength include ISO 3597, 12579, and 14130.^[7]

References

^ Hibbeler, Russell (9 November 2017). Mechanics of materials. Pearson Education. ISBN 978-1-292-17828-8. OCLC 1014358513.
^ "Mechanics eBook: Shear and Bearing Stress". www.ecourses.ou.edu. Retrieved 2020-02-14.
^ "Shear Strength of Metals". www.roymech.org.
^ "Shear Strength - Instron". www.instron.us. Archived from the original on 2020-02-14. Retrieved 2020-02-14.
^ Portl; Portl, bolt com; Bolt; Company, Manufacturing; St, Inc 3441 NW Guam; Portl; PT547-6758, OR 97210 USA Hours: Monday-Friday 6 AM to 5 PM (10 October 2011). "Calculating Yield & Tensile Strength". Portland Bolt. Retrieved 2020-02-14. {{cite web}}: |last4= has generic name (help)CS1 maint: numeric names: authors list (link)
^ Watson, DC (May 1982). Mechanical Properties of E293/1581 Fiberglass-Epoxy Composite and of Several Adhesive Systems (PDF) (Technical report). Wright-Patterson Air Force, Ohio: Air Force Wright Aeronautical Laboratories. p. 16. Archived (PDF) from the original on 24 October 2018. Retrieved 24 October 2013.
^ S. Grynko, "Material Properties Explained" (2012), ISBN 1-4700-7991-7, p. 38.