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TECHNICAL BRIEF

Interface Properties Due to Microslip From Vibration Measurement

[+] Author and Article Information
H. A. Sherif

Department of Engineering Mechanics, Military Technical College, Cairo, Egypt

T. M. Abu Omar

Department of Aircraft, Military Technical College, Cairo, Egypt

J. Tribol 123(1), 230-233 (Nov 04, 1999) (4 pages) doi:10.1115/1.1286171 History: Received May 05, 1999; Revised November 04, 1999
Copyright © 2001 by ASME
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References

Figures

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Contact of sub-structures and their mathematical model of microslip
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Effect of contact stiffness kt on the amplitude ratio: (a) magnitude; (b) phase
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Experimental setup and devices (CA=conditioning amplifier; A, B=accelerometers;DD=disc drive; N=load weight; SA=signal analyzer; PL=x-y plotter)
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Effect of normal load on the amplitude ratio: (a) magnitude; (b) phase
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Variation of contact stiffness kt and loss factor η with the normal load N for two different positions of contact

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