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A Comparison of Helicopter Main Rotor Features Due to Stiffness of Rotor Blade-Hub Connection Cover

A Comparison of Helicopter Main Rotor Features Due to Stiffness of Rotor Blade-Hub Connection

Transactions on Aerospace Research
Volume 2018 (2018): Issue 1 (March 2018)
By: Jarosław Stanisławski  
Open Access
|Jul 2019

Authors

Jarosław Stanisławski

jaroslaw.stanislawski@ilot.edu.pl

Institute of Aviation, Warsaw, Poland
DOI: https://doi.org/10.2478/tar-2018-0008 | Journal eISSN: 2545-2835
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Language: English
Page range: 119 - 136
Published on: Jul 25, 2019
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year
Keywords:
helicopter,
main rotor,
blade deformations
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other,
Geosciences,
Geosciences, other,
Materials sciences,
Materials sciences, other,
Physics,
Physics, other

© 2019 Jarosław Stanisławski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

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