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Design and Strength Analysis of Curved-Root Concept for Compressor Rotor Blade in Gas Turbine Cover

Design and Strength Analysis of Curved-Root Concept for Compressor Rotor Blade in Gas Turbine

Fatigue of Aircraft Structures
Volume 2017 (2017): Issue 9 (December 2017)
By: Wojciech Wdowiński,  Elżbieta Szymczyk,  Jerzy Jachimowicz and  Grzegorz Moneta  
Open Access
|Aug 2018
Authors

Authors

Wojciech Wdowiński

Ansaldo Energia, Switzerland

Elżbieta Szymczyk

Military University of Technology, Warsaw

Jerzy Jachimowicz

Military University of Technology, Warsaw

Grzegorz Moneta

Ansaldo Energia, Switzerland
DOI: https://doi.org/10.1515/fas-2017-0011 | Journal eISSN: 2300-7591
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Language: English
Page range: 137 - 155
Published on: Aug 9, 2018
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
finite element method,
turbine engine,
rotor disk,
rotor blades,
blade-disc connection,
shape optimization
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2018 Wojciech Wdowiński, Elżbieta Szymczyk, Jerzy Jachimowicz, Grzegorz Moneta, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Volume 2017 (2017): Issue 9 (December 2017)
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