Case Study and Simulation of Fatigue Damages and DTE of Aging Aircraft — A Review of Researches in Japan

  • H. Terada
  • K. Ohtsuka
Conference paper
Part of the Springer Series in Computational Mechanics book series (SSCMECH)


This is a review paper on the study of aging aircraft structures conducted in Japan.


Fatigue Crack Laminate Plate Joint Specimen National Aerospace Laboratory Rivet Hole 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.


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  1. [1]
    Kamiyama, T., Takeuchi, K., Shima, F., and Kitatani, K. “Full-Scale Fatigue Test of Twin-turboprop Transport”, Experimental Mechanics, SESA, April, 1966, pl94.Google Scholar
  2. [2]
    Shiohara, T., Uchimoto, T. and Koga, K., “Development of SID on YS-11 Twin-Turboprop Transport for Continuing Structural Integrity of High Time Airplanes”, Proceeding of ICOSSAR’ 85, IASSAR, May, 1985, VOL. 11, pll7.Google Scholar

Copyright information

© Springer-Verlag Berlin, Heidelberg 1991

Authors and Affiliations

  • H. Terada
    • 1
  • K. Ohtsuka
    • 2
  1. 1.National Aerospace Laboratorychofu TokyoJapan
  2. 2.Association of Air Transport Engineering and ResearchMinato-ku TokyoJapan

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