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Stress Intensity Factor Calculations for the Compressor Blade with Half-Elliptical Surface Crack Using Raju-Newman Solution Cover

Stress Intensity Factor Calculations for the Compressor Blade with Half-Elliptical Surface Crack Using Raju-Newman Solution

By: Lucjan Witek  
Open Access
|Aug 2011

References

  1. Newman, J.C. Jr. & Raju, I.S. (1981). An empirical stress intensity factor equation for surface cracks. Engineering Fracture Mechanics, Vol. 15, pp. 185-192.10.1016/0013-7944(81)90116-8
  2. Barlow, K.W. & Chandra, R. (2005). Fatigue crack propagation simulation in an aircraft engine fan blade attachment. International Journal of Fatigue 27(10-12), 1661-1668.10.1016/j.ijfatigue.2005.06.016
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  7. Witek, L. (2009). Experimental crack propagation and failure analysis of the first stage compressor blade subjected to vibration. Engineering Failure Analysis. 16(7), 2163-2170.10.1016/j.engfailanal.2009.02.014
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DOI: https://doi.org/10.2478/v10164-010-0046-2 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 154 - 165
Published on: Aug 25, 2011
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2011 Lucjan Witek, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

Volume 2011 (2011): Issue 3 (August 2011)