Search Results

Search Results

• Comparison between two and three parameters of fatigue crack growth models in airframe structures

  Muhammad Shujauddin Wahab, Yuri M. Paramonov

  Abstract 749 | PDF Downloads 536 | DOI https://doi.org/10.3846/16487788.2005.9635899

  Page 17-23
  

  2005-06-30

• Inspection program development for fatigue crack growth model with two random parameters

  Yuri Paramonov, Andrey Kuznetsov

  Abstract 726 | PDF Downloads 537 | DOI https://doi.org/10.3846/1648-7788.2008.12.33-40

  Page 33-40
  

  2008-06-30

• Reliability of fleet of aircraft taking into account information exchange about the discovery of fatigue cracks and the human factor

  Yuri Paramonov, Sergey Tretyakov

  Abstract 778 | PDF Downloads 552 | DOI https://doi.org/10.3846/16487788.2012.753680

  Page 103-108
  

  2012-12-24

• The influence of corrosion on reliability and inspection program for fatigue‐prone airframe structures

  M. Shujauddin Wahab, Yuri M. Paramonov

  Abstract 781 | PDF Downloads 535 | DOI https://doi.org/10.3846/16487788.2004.9635876

  Page 10-17
  

  2004-09-30

• Aproximation of fatigue curve and fatigue limit of fibre composite using random Daniels’ sequence and Markov chains

  Yuri Paramonov, Vjacheslavs Cimanis, Sergejs Varickis

  Abstract 868 | PDF Downloads 734 | DOI https://doi.org/10.3846/16487788.2013.840071

  Page 91-97
  

  2013-10-07

• Binomial version of Markov model of fatigue life of composite with two reasons for failure

  Alexandra Paramonova, Martinsh Kleinhofs, Yuri Paramonov

  Abstract 802 | PDF Downloads 547 | DOI https://doi.org/10.3846/16487788.2004.9635870

  Page 14-20
  

  2004-06-30