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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DOI: 10.3390/aerospace6120132
Published: 2019-12-09
Container: Aerospace
Publisher: MDPI AG
Open access: unknown

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Cite this work

BibTeX

@article{allodium:10.3390/aerospace6120132,
  title = {Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin},
  author = {Yaroslav Dvirnyk and Dmytro Pavlenko and Radoslaw Przysowa},
  year = {2019},
  journal = {Aerospace},
  doi = {10.3390/aerospace6120132},
  url = {https://doi.org/10.3390/aerospace6120132}
}

RIS

TY  - JOUR
TI  - Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin
AU  - Yaroslav Dvirnyk
AU  - Dmytro Pavlenko
AU  - Radoslaw Przysowa
PY  - 2019
JO  - Aerospace
DO  - 10.3390/aerospace6120132
UR  - https://doi.org/10.3390/aerospace6120132
ER  -

APA

Dvirnyk, Y., Pavlenko, D., & Przysowa, R. (2019). Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin. Aerospace. https://doi.org/10.3390/aerospace6120132

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crossref · retrieved 2026-11-10T14:00:01.447Z