Discussion: “A Paradox in Sliding Contact Problems With Friction” (Adams, G. G., Barber, J. R., Ciavarella, M., and Rice, J. R., 2005, ASME J. Appl. Mech., 72, pp. 450–452) OPEN ACCESS

[+] Author and Article Information
D. A. Hills1

Department of Engineering Science,  University of Oxford, Parks Road, Oxford OX1 3PJ, UKdavid.hills@eng.ox.ac.uk

A. Sackfield, C. M. Churchman

Department of Engineering Science,  University of Oxford, Parks Road, Oxford OX1 3PJ, UK


Author to whom correspondence should be addressed.

J. Appl. Mech 73(5), 884-886 (Sep 01, 2006) (3 pages) doi:10.1115/1.2201886 History:

In this interesting paper, the authors address an anomaly which arises when a rigid, square-ended block is pressed against a linear elastic half plane and slid along. The authors note that, within the framework of linear elasticity, the singularity in the contact pressure, and hence shearing traction, produces, adjacent to the edges, regimes in which the implied local relative slip direction dominates the rigid-body sliding velocity, and hence produces a violation of the Coulomb friction law. They seek to resolve the paradox by appealing to a more sophisticated strain definition. All of this is within the context of a quasistatic formulation. The authors recognize, of course, that in any real problem the paradox is unlikely to arise because of (a) the finite strength of the contact giving rise to a yield zone, and (b) the absence of an atomically sharp corner at the contact edge where there is, in all probability, a finite edge radius. Here, we wish to address these issues quantitatively, and so demonstrate that it is unlikely that the paradox described, though interesting, will have any bearing in a real contact.

The punch is moving at velocity U0 in the positive x direction, relative to the half plane (with the coordinate system (x,y) moving with it), and the surface normal displacement, v(x), and tangential displacement, u(x), are given byDisplay Formula

Display Formula
whereDisplay Formula
ν being the Poisson’s ratio and μ the modulus of rigidity of the half plane. The slip velocity of particles on the punch surface relative to particles on the half-plane surface, U(x), is given in the original paper byDisplay Formula
As the contact is sliding the tractions are related everywhere by q(x)=fp(x), where f is the coefficient of friction, so that Eq. 1 becomesDisplay Formula
and from Eq. 2 we haveDisplay Formula
Therefore, the surface normal displacements and surface tangential displacements are given byDisplay Formula
and hence the relative slip velocity isDisplay Formula
The slip direction is reversed when UUo>1.

Because the region of apparent reverse slip is so small the problem can conveniently be readdressed using an asymptote which gives the problem additional simplicity and applicability. Suppose that a rigid quarter plane is pressed onto the elastic half plane and slid in the positive x direction, with friction. The local contact pressure, p(s), and shearing traction, q(s), may be written in the form (1)Display Formula

where KN is a generalized stress intensity factor and s is a coordinate measured from the contact edge. The exponent, λ, is given by the characteristic equationDisplay Formula
We now turn our attention to the finite, flat-ended rigid punch, of half-width a, to which a normal load, P, is applied, together with a force sufficient to cause sliding in the positive x direction. This develops a contact pressure, p(x), (2) given byDisplay Formula
such that p(x) is positive in compression. If we apply the change of coordinate sa=1+xa we getDisplay Formula
Display Formula
where we have introduced an average pressure po=P2a, and henceDisplay Formula
We now apply the relationship for the slip velocity U(x) to this solution where, of course, dvdx=0, and the region where the implied slip direction is reversed is whenDisplay Formula
i.e., over a region s<e whereDisplay Formula
Therefore, for this specific geometry, when we employ the calibration for KN, the reversal in slip direction occurs over a region s<e whereDisplay Formula
Thus, the phenomenon presented in the original paper occurs whenever the half plane has a finite compressiblity (ν<12), even if no shearing tractions arise (f=0), but clearly the region of violation increases in size with (a) friction, (b) reduced Poisson effect, (c) dimensionless contact pressure (poμ). The most extreme values one might expect to encounter in practice might be a Poisson’s ratio of 0.2, a coefficient of friction of 0.8, and a mean contact pressure of poμ=0.001, giving λ=0.41, so thatDisplay Formula
which is itself tiny, and readily swamped by local plasticity or the effects of rounding.

We turn now to the question of envelopment of the region of reverse slip by plasticity. As the complete stress field associated with the asymptote is known, through the Muskhelishvili potential, it is straightforward to establish an estimate of the size of the edge plastic zone, simply by seeing where the yield condition is exceeded, in the spirit of the usual fracture mechanics crack-tip plasticity correction.

The Muskhelishvili potential for a rigid punch on a half plane is given byDisplay Formula

where z=s+iy is a complex coordinate in the half plane (and i=1). The second invariant of the stress tensor as described by von Mises’ equivalent stress is (along the interface, y=0)Display Formula
and yield is expected to occur when σe=σY=3τY. This condition is satisfied over a region s<rp, where rp isDisplay Formula
and again using the calibration for KN from the finite geometryDisplay Formula
which for ν=0.2,f=0.8, and σYμ=3×103 (hence poσY=13) givesDisplay Formula
Thus, for this contact pressure, there will be plasticity over a region roughly 105 times larger than the zone over which the paradox occurs.

To probe the effect of edge rounding we consider sliding contact between another rigid semi-infinite punch pressed onto the half plane and sliding. This time, contact is assumed to extend from d<x<, and the surface displacement gradient is defined byDisplay Formula

Display Formula
i.e., the indenter has the form of a parabolic arc of equivalent radius R to the left of the origin, and is flat to the right of the origin. This profile is substituted into integral Eqs. 1 and 2 and solved, giving a pressure along the interface ofDisplay Formula
Display Formula
where s=x+d and F12(.) is a standard hypergeometric function. We note that, when (sd)1, p(x)sλ1, so that the asymptotic form given by Eq. 27 applies, and calibration shows that the generalized stress intensity factor is given byDisplay Formula
This scaling factor serves both to provide a connection between the applied load (KN) and the extent of contact in the radiused portion, d, and it enables us to write the contact pressure asDisplay Formula
Display Formula
whereas the relative slip displacement is given byDisplay Formula
Display Formula
and, employing the contact law for this problem,Display Formula
givesDisplay Formula
Display Formula
Therefore there is a violation in slip direction when UU0>1, i.e., whenDisplay Formula
The violation is more likely to occur for cases when R2a is very small and the load poμ is relatively high. However, unlike the perfectly sharp solution, the function Ψ(sd,f,β) does not exhibit a monotonically increasing value as s0 but shows a maximum. This cannot be found analytically, but has been found numerically for the extreme example case used earlier (f=0.8, ν=0.2) so that the maximum of Ψ(sd,f,β) occurs at sd=0.133 and is of magnitude 1.002. Therefore, using the same load as before, poμ=0.001, we find that the paradox will occur ifDisplay Formula
If we have a contact of total width 20mm then in order to avoid the paradox occurring we require R>120nm. This is such a tiny radius that for all contacts of practical importance the paradox will not exist.

The region of reverse slip violating the friction law has been quantified and shown to be extremely small. Physical boundaries for its envelopment by plasticity or absence through local rounding have also been explicitly found. It is very probable that plasticity will produce the greater effect.

Copyright © 2006 by American Society of Mechanical Engineers
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