publication . Preprint . Other literature type . Article . 2019

Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin

Dmytro Pavlenko; Yaroslav Dvirnyk; Radosław Przysowa;
Open Access English
  • Published: 09 Dec 2019
  • Publisher: Preprints
790 flight hours. In addition, recommendations setting out go/no-go criteria are made to maintenance and repair organizations.
free text keywords: mechanical_engineering, gas-turbine performance, turboshaft, axial compressor, blade, FEM, CFD, erosion, wear, stall margin, compressor surge, brownout, Stall (fluid mechanics), Structural engineering, business.industry, business, Environmental science, Natural frequency, Serviceability (structure), Campbell diagram, Compressor stall, Vibration, Computer science, lcsh:Engineering (General). Civil engineering (General), lcsh:TA1-2040
Related Organizations
Funded by
Strategic and Targeted Support for Europe-Ukraine Collaboration in Aviation Research
  • Funder: European Commission (EC)
  • Project Code: 724034
  • Funding stream: H2020 | CSA

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