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 900 | PDF Downloads 596 | DOI https://doi.org/10.3846/16487788.2005.9635899

  Page 17-23
  

  2005-06-30

• Blade element – momentum aerodynamic model of a helicopter rotor operating at low-Reynolds numbers in ground effect

  Gabriel Georgiev

  Abstract 1132 | PDF Downloads 569 | DOI https://doi.org/10.3846/aviation.2025.23587

  Page 71–81
  

  2025-05-21

• Use of statistical reference method to improve flight safety

  Irina Lazareva, Vladimir Shestakov

  Abstract 935 | PDF Downloads 628 | DOI https://doi.org/10.3846/16487788.2012.701864

  Page 42-46
  

  2012-06-29