Effects of microstructure on mixed-mode, high-cycle fatigue crack-growth thresholds in Ti-6Al-4V alloy-Reference-Cited by-同舟云学术

Effects of microstructure on mixed-mode, high-cycle fatigue crack-growth thresholds in Ti-6Al-4V alloy

Published:2002-05-21 Issue:6 Volume:25 Page:587-606
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:

Author:

Nalla R. K.,Campbell J. P.,Ritchie R. O.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1046/j.1460-2695.2002.00522.x/fullpdf

Reference49 articles.

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2. High-cycle fatigue in aircraft gas turbines - an industry perspective;Cowles;Int. J. Fract,1996

3. Chang , J. C. I. 1996 Air Force Office of Scientific Research, Bolling AFB

4. Multidisciplinary University Research Initiative on High-Cycle Fatigue. Air Force Office of Scientific Research

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