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

Data publikacji: 09 sie 2018

Zakres stron: 137 - 155

DOI: https://doi.org/10.1515/fas-2017-0011

Słowa kluczowe

finite element method, turbine engine, rotor disk, rotor blades, blade-disc connection, shape optimization

© 2017 Wojciech Wdowiński et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.