
chip formation. Repeated-cycle deformation wear results from the accumulation of plastic
strain associated with the stress cycle, culminating in progressive plastic deformation,
crack formation, and crack propagation.
This consideration of hysteretic friction points out a significant aspect of friction,
namely that it results in the dissipation of energy. The energy associ ated with friction is
dissipated in two general ways. The vast majority of the energy is dissipated as heat
(3–5). A much smaller amount is associated with material loss or deformation, that is,
wear. Most estimates indicate that well over 90% of the energy dissipated in friction goes
in the form of heat energy.
Models have been proposed for these friction mechanisms but are typically limited
in applicability. Generally, all of the models indicate a more complex situation than indi-
cated by the postulations of da Vinci and Amontons (ca. 1500 and 1700, respectively)
which frequently are used in engineering. These statements, commonly referred to as
Amontons’ Laws of Friction, may be summarized as: (1) the friction force is propor-
tional to the normal load, (2) the friction force is independent of the apparent area of
contact. The current models, as well as experimental data, indicate that these conclu-
sions should be viewed as approximations with a limited range of applicability. This
view can be illustrated by the consideration of some simple models for friction force
and the coefficient of friction and some examples of observed behavior. For simplicity,
only dry or unlubricated surfaces will be considered at this point. Friction behavior
under lubricated conditions will be discussed in the section on lubrication. A model used
for paper can be used as a way of illustrating these general models (6).
For adhesion, the general concept is that the F
ad
is given by
F
ad
¼ sA
r
ð5:4Þ
where s is the shear strength of the junctions, and A
r
is the real area of contact (7). s is a
property of the material system at the interface and is influenced by the same parameters
as discussed for adhesive wear (e.g., oxides, cleanliness of the surface, solubility, material
strength properties). As was discussed in the sections on wear, A
r
can be affected by mate-
rial properties, asperity distribution, and contact geometry. For example, in the case of a
sphere pressed against a plane, a general relationship for A
r
is of the following form:
A
r
¼ CR
n
P
m
ð5:5Þ
where C is a material parameter, R is the radius of the sphere, and P is the normal load
(8,9). The exponents, n and m, are positive and depend on both the nature of the stress
system at the junctions and the asperity distribution. For plastic deformation, n ¼ 0
and m ¼ 1. For elastic deformation, n > 0 and m is between 0 and 1 for relatively simple
asperity distributions but can be greater than 1 for some complex asperity distributions.
The expression for the coefficient of friction then has the following form:
m
ad
¼ K
ad
R
n
P
m1
ð5:6Þ
where C and s are combined into K
ad
. Implicit in this relationship is the additional depen-
dencies on load and other parameters as a result of their ability to influence tribosurfaces.
These would be contained in K
ad
.
Abrasive fric tion can be illustrated by considering a cone of included angle F plowing
through a softer surface. For plastic deformation, the force required to do this, F
0
, is given by
F
0
¼
cot FP
0
p
ð5:7Þ
Copyright 2004 by Marcel Dekker, Inc. All Rights Reserved.