Search Results

Search Results

• Numerical model of aviation gearbox test rig in a closed loop configuration

  Tadeusz Markowski, Stanislaw Noga, Stanislaw Rudy

  Abstract 751 | PDF Downloads 578 | DOI https://doi.org/10.3846/aviation.2010.01

  Page 3-11
  

  2010-03-31

• Progressive failure analysis of helicopter rotor blade under aeroelastic loading

  Kamran Ahmad , Yasir Baig , Hammad Rahman , Hassan Junaid Hasham

  Abstract 2017 | PDF Downloads 1237 | DOI https://doi.org/10.3846/aviation.2020.12184

  Page 33-41
  

  2020-04-23

• Numerical analysis of the impact of sideslip angle on load of the gyrocopter stabilizers

  Zbigniew Czyż , Paweł Karpiński

  Abstract 1807 | PDF Downloads 1135 | DOI https://doi.org/10.3846/aviation.2019.11924

  Page 114-122
  

  2019-12-31

• Reduction of the vibration in a helicopter blade using piezoelectric actuators

  Sergejs Gluhihs, Andrejs Kovalovs

  Abstract 725 | PDF Downloads 543 | DOI https://doi.org/10.3846/16487788.2006.9635927

  Page 3-6
  

  2006-06-30