Shear stress
Shear stress is the component of stress coplanar with a material cross section. It arises from the shear force, the component of force vector parallel to the material cross section. Normal stress, on the other hand, arises from the force vector component perpendicular to the material cross section on which it acts.
General shear stress
The formula to calculate average shear stress or force per unit area is:where is the force applied and is the cross-sectional area.
Other forms
Wall shear stress
Wall shear stress expresses the retarding force from a wall in the layers of a fluid flowing next to the wall. It is defined as:where is the dynamic viscosity, is the flow velocity, and is the distance from the wall.It is used, for example, in the description of arterial blood flow, where there is evidence that it affects the atherogenic process.
Pure
stress is related to pure shear strain, denoted, by the equationwhere is the shear modulus of the isotropic material, given byHere, is Young's modulus and is Poisson's ratio.Beam shear
Beam shear is defined as the internal shear stress of a beam caused by the shear force applied to the beam:whereThe beam shear formula is also known as Zhuravskii shear stress formula after Dmitrii Ivanovich Zhuravskii, who derived it in 1855.
Semi-monocoque shear
Shear stresses within a semi-monocoque structure may be calculated by idealizing the cross-section of the structure into a set of stringers and webs. Dividing the shear flow by the thickness of a given portion of the semi-monocoque structure yields the shear stress. Thus, the maximum shear stress will occur either in the web of maximum shear flow or minimum thickness.Constructions in soil can also fail due to shear; e.g., the weight of an earth-filled dam or dike may cause the subsoil to collapse, like a small landslide.
Impact shear
The maximum shear stress created in a solid round bar subject to impact is given by the equationwhereFurthermore,
,
where
Shear stress in fluids
Any real fluids moving along a solid boundary will incur a shear stress at that boundary. The no-slip condition dictates that the speed of the fluid at the boundary is zero, although at some height from the boundary, the flow speed must equal that of the fluid. The region between these two points is named the boundary layer. For all Newtonian fluids in laminar flow, the shear stress is proportional to the strain rate in the fluid, where the viscosity is the constant of proportionality. For non-Newtonian fluids, the viscosity is not constant. The shear stress is imparted onto the boundary as a result of this loss of velocity.For a Newtonian fluid, the shear stress at a surface element parallel to a flat plate at the point is given bywhere
Specifically, the wall shear stress is defined asNewton's constitutive law, for any general geometry, states that shear tensor is proportional to the flow velocity gradient :The constant of proportionality is named dynamic viscosity. For an isotropic Newtonian flow, it is a scalar, while for anisotropic Newtonian flows, it can be a second-order tensor. The fundamental aspect is that for a Newtonian fluid, the dynamic viscosity is independent of flow velocity, while for non-Newtonian flows this is not true, and one should allow for the modificationThis no longer Newton's law but a generic tensorial identity: one can always find an expression of the viscosity as function of the flow velocity given any expression of the shear stress as function of the flow velocity. On the other hand, given a shear stress as function of the flow velocity, it represents a Newtonian flow only if it can be expressed as a constant for the gradient of the flow velocity. The constant one finds in this case is the dynamic viscosity of the flow.