Numerical Modeling of Dynamic Friction Phenomena
New Micro- and Macroscopic Models of Contact and
Friction
Sponsored by: The Air Force Office
of Scientific Research
Project duration: 1986-1993
These projects, which were sponsored over
many years by the Air Force Office of Scientific Research, were dedicated
to understanding, modeling and prediction of phenomena of dynamic friction,
in particular of friction-induced oscillations, squeaks, stick-slip motion,
and the difference between the static and kinetic coefficient of friction.
Importantly, these complex phenomena have been a subject of numerous experimental,
theoretical and numerical studies. Until recently, most of these studies
had a very limited success, in that no general understanding and modeling
methodology were developed for the stick-slip, squeak, chatter and related
phenomena. Some previous approaches based on velocity-dependence of friction
were partially successful in explaining selected cases and in modeling
selected apparatus, but were not general enough to represent a wide class
of friction-induced oscillations. In particular, it was observed that the
results obtained on one apparatus usually did not transfer to a different
setup, even with the same frictional samples. For a review of these and
other efforts, see an exhaustive paper by Ibrahim [1]. During the course
of the project, new understanding of these phenomena was developed and
a new models of contact and friction were formulated. Some of the most
important findings of this research [2,3,4] are listed as follows:
-
Contrary to intuition of many investigators
in the past, it is the normal compliance rather than tangential properties
of the interface that must be modeled adequately to capture the appropriate
friction phenomena. The authors of this summary have formulated new phenomenological
models of contact and friction (Oden-Martins model [2]) which take into
account both normal and tangential properties of the interface. These models
are capable of delivering results in good correlation with experimental
observations.
-
A basic mechanism of self-excited frictional
oscillations for mechanical systems has been identified as unstable, friction-induced
vibrations triggered by coupling between normal and rotational motion of
the components of the sliding system, with additional presence of velocity-dependence
of the coefficient of friction [3]. This conclusion is in accord with recent
experimental observations of Dweib and D'souza, and has been used successfully
in modeling of friction-induced oscillations of representative mechanical
systems.
-
A new class of asperity-based models of frictional
interfaces has been developed [4]. These models combine accurate finite
element analysis of micro-scale asperities with statistical homogenization
methods, to produce macro-scale models of contact and friction. Such an
approach provides a new insight into the phenomena occurring on frictional
interfaces and defines a new class of constitutive interface models, consistent
with both micro-scale behavior and macro-scale phenomenological observations.
As a result, COMCO has presently a leading
edge expertise in numerical simulation and prediction of friction-induced
vibrations. This expertise is presently being used in practical industrial
applications.
References:
-
[1] Ibrahim, R.A., "Friction-Induced Vibration,
Chatter, Squeal and Chaos", ASME Mechanics Reviews, 47, 7, 1994, pp. 209-253.
-
[2] Oden, J.T. and Martins, J.A.C, "Models
and Computational Methods for Dynamic Friction Phenomena", Comp. Meth.
Appl. Mech. Engng., 52, 1985, pp. 527-634.
-
[3] Tworzydlo, W.W., Becker, E.B. and Oden,
J.T., "Numerical Modeling of Friction-Induced Vibrations and Dynamic Instabilities",
ASME Mechanics Reviews, 47, 7, 1994, pp. 255-274
-
[4] Tworzydlo, W.W., Cecot, W., Oden, J.T.
and Yew, C.H., "New Asperity-Based Models of Contact and Friction", in
Contact Problems and Surface Interactions in Manufacturing and Tribological
Systems, eds. Attia, M.H. and Komanduri, R., TRIB, Vol. 4., ASME, 1993.
Questions, comments or problems regarding this service? webmaster@tx.altair.com.
Copyright 2000
Altair Engineering, Inc.