Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin
Dvirnyk, Y.; Pavlenko, D.; Przysowa, R. Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin. Aerospace 2019, 6, 132. https://doi.org/10.3390/aerospace6120132
Dvirnyk Y, Pavlenko D, Przysowa R. Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin. Aerospace. 2019; 6(12):132. https://doi.org/10.3390/aerospace6120132
Chicago/Turabian StyleDvirnyk, Yaroslav, Dmytro Pavlenko, and Radoslaw Przysowa. 2019. "Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin" Aerospace 6, no. 12: 132. https://doi.org/10.3390/aerospace6120132