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Effects of Phase Difference Between Axial and Contact Loads on Fretting Fatigue Behavior of Titanium Alloy

Effects of Phase Difference Between Axial and Contact Loads on Fretting Fatigue Behavior of Titanium Alloy

Effects of Phase Difference Between Axial and Contact Loads on Fretting Fatigue Behavior of Titanium Alloy Paperback - 2012

by Mohammad Almajali

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Paperback. New. New Book; Fast Shipping from UK; Not signed; Not First Edition; Fretting fatigue is the surface damage that occurs at the interface between two components that are undergoing a small amplitude oscillatory movements. It results in a reduction of the material life as compared to the plain fatigue. Mos
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Details

  • Title Effects of Phase Difference Between Axial and Contact Loads on Fretting Fatigue Behavior of Titanium Alloy
  • Author Mohammad Almajali
  • Binding Paperback
  • Condition New
  • Pages 168
  • Volumes 1
  • Language ENG
  • Publisher Biblioscholar
  • Publication date 2012-12-04
  • Bookseller's Inventory # ria9781288398744_inp
  • ISBN 9781288398744 / 1288398743
  • Weight 0.69 lbs (0.31 kg)
  • Dimensions 9.69 x 7.44 x 0.36 in (24.61 x 18.90 x 0.91 cm)
  • Category Education / Teaching
  • Quantity available 796

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Reader reviews for Effects of Phase Difference Between Axial and Contact Loads on Fretting Fatigue Behavior of Titanium Alloy

From the publisher

Fretting fatigue is the surface damage that occurs at the interface between two components that are undergoing a small amplitude oscillatory movements. It results in a reduction of the material life as compared to the plain fatigue. Most of the previous works were accomplished under a constant applied normal load and a little effort was done under a variable contact load, while none of these studies has considered the phase difference between the axial load and the contact load. The primary goal of this study is to investigate the effect of phase difference between axial and contact loads on fretting fatigue behavior of Ti-6Al-4V alloy. The frequency of both axial and contact loads was the same. i.e. 10 Hz. Under variable contact load condition; only the axial stress range and the phase angle were varied.

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