Materials Science

, Volume 47, Issue 5, pp 621–626 | Cite as

Application of Fractal Geometry to the Problems of Prediction of the Residual Service Life of Aircraft Structures

  • M. V. Karuskevych
  • I. M. Zhuravel’
  • T. P. Maslak

The deformation pattern of the surface of clad aluminum alloys is regarded as an indicator of the degree of accumulated fatigue damage. We demonstrate the possibility of application of the methods of fractal geometry to the analysis of the optical images of deformation patterns. We study a series of procedures used for the calculation of fractal dimensions and propose their complex application to the problems of prediction of the residual service life of aircraft structures according to the state of the deformation pattern.


aircraft structures clad aluminum alloy fatigue damage residual service life deformation pattern fractal dimension 


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Copyright information

© Springer Science+Business Media, Inc. 2012

Authors and Affiliations

  • M. V. Karuskevych
    • 1
  • I. M. Zhuravel’
    • 2
  • T. P. Maslak
    • 1
  1. 1.National Aviation UniversityKyivUkraine
  2. 2.Karpenko Physicomechanical Institute, Ukrainian National Academy of SciencesLvivUkraine

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