Journal article Open Access
Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin
Yaroslav Dvirnyk; Dmytro Pavlenko; Radoslaw Przysowa
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| Data volume | 107.8 MB |
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Indexed in
- Publication date:
- December 9, 2019
- DOI:
-
- Keyword(s):
- gas-turbine performance turboshaft axial compressor blade FEM CFD erosion wear stall margin compressor surge brownout
- Grants:
-
European Commission:
- AERO-UA - Strategic and Targeted Support for Europe-Ukraine Collaboration in Aviation Research (724034)
- License (for files):
- Creative Commons Attribution 4.0 International