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 680 | PDF Downloads 521 | DOI https://doi.org/10.3846/16487788.2005.9635899

  Page 17-23
  

  2005-06-30

• Model of acoustic emission signal at self‐accelerated crack development

  Vitalii Babak, Sergay Filonenko, Viktor Kalita

  Abstract 782 | PDF Downloads 532 | DOI https://doi.org/10.3846/16487788.2005.9635904

  Page 3-8
  

  2005-09-30

• Estimation of warranty period for structural components of aircraft

  Nicholas A. Nechval, Konstantin N. Nechval, Edgars Vasermanis

  Abstract 765 | PDF Downloads 507 | DOI https://doi.org/10.3846/16487788.2004.9635875

  Page 3-9
  

  2004-09-30

• Stress analysis of turbine components under spin rig thermomechanical condition

  Lucjan Witek

  Abstract 776 | PDF Downloads 1855 | DOI https://doi.org/10.3846/16487788.2004.9635885

  Page 21-26
  

  2004-12-31

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

  M. Shujauddin Wahab, Yuri M. Paramonov

  Abstract 765 | PDF Downloads 528 | DOI https://doi.org/10.3846/16487788.2004.9635876

  Page 10-17
  

  2004-09-30

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

  Yuri Paramonov, Andrey Kuznetsov

  Abstract 710 | PDF Downloads 530 | DOI https://doi.org/10.3846/1648-7788.2008.12.33-40

  Page 33-40
  

  2008-06-30