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  4. Analysis of multiple crack propagation in stiffened sheet.
 
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1991
Conference Paper
Title

Analysis of multiple crack propagation in stiffened sheet.

Other Title
Mehrfachrisse in versteiften Hautfeldern
Abstract
A model for crack growth prediction in stiffened sheets and joints with multiple cracks is presented. To determine the stress intensity factors, interactions between cracks, load redistribution, and influences of holes on cracks are considered. Limitations of the model are briefly discussed. The applicability of the model is demonstrated on configurations available in the literature and results are compared with data from crack growth experiments.
Author(s)
Lehrke, H.-P.
Schöpfel, A.
Mainwork
Aeronautical fatigue - key to safety and structural integrity. Proceedings  
Conference
International Committee on Aeronautical Fatigue (Symposium) 1991  
Language
English
Fraunhofer-Institut für Betriebsfestigkeit und Systemzuverlässigkeit LBF  
Keyword(s)
  • aircraft industry

  • crack propagation

  • crack propagation prediction

  • damage tolerance

  • experiment

  • fatigue strength

  • Flugzeugbau

  • Mehrfachriss

  • multiple crack

  • Nietverbindung

  • residual strength

  • Restfestigkeit

  • Rißfortschritt

  • Rißfortschrittsvorhersage

  • riveted joint

  • Schadenstoleranz

  • Schwingfestigkeit

  • Spannungsintensitätsfaktor

  • stiffener

  • stress intensity factor

  • Versteifung

  • Versuch

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