Effects of damping on brake squeal coalescence patterns – application on a finite element model
✍ Scribed by Guillaume Fritz; Jean-Jacques Sinou; Jean-Marc Duffal; Louis Jézéquel
- Publisher
- Elsevier Science
- Year
- 2007
- Tongue
- English
- Weight
- 628 KB
- Volume
- 34
- Category
- Article
- ISSN
- 0093-6413
No coin nor oath required. For personal study only.
✦ Synopsis
Brake squeal is referred to, in most publications, as a flutter instability triggered by a mode coupling phenomenon. A lot of clues tend to prove that damping would be a key parameter in brake squeal modelling. This study aims at investigating the effects of damping on coalescence patterns, that is to say on the way the modes couple. A finite element model of the whole brake corner has been used to compute the brake modal behaviour. Then a complex eigenvalue analysis has been undertaken to assess the brake stability as a function of the friction coefficient. Different kinds of damping spreading over the modes have been studied. Two main effects have been noticed: a shifting effect and a smoothing effect. The first one always stabilize the brake, whereas this is not the case of the second one. The combination of the two effects may make the brake more unstable depending on the spreading of the additionnal damping.
📜 SIMILAR VOLUMES
A finite element model of a rotor-bearing system with non-axisymmetric stiffness and mass properties was analyzed in a previous study. In this paper the model is extended to include the effects of external damping due to symmetrical tilting-pad bearings. The same instability mechanisms, due to the l
Dynamic wetting plays an important role in coating processes. In this paper, we present a new finite element formulation that can predict the effect of substrate deformation on the location of the dynamic contact line. Our model solves for the fluid-structural interactions between an elastic solid a
Finite element methods are used extensively to study the behaviour of complex structures [1,2]. When several finite elements must be considered to model a structure due to spatial variations in its properties, the number of nodal co-ordinates becomes very large and the eigenvalue problem becomes ver
The recent interest in propeller noise generation, stimulated by development of new propeller types for commercial propjets, has generated a need for the ability to measure the noise characteristics of propellers. However, wind tunnel noise measurements are affected by reflections from the wind tunn