Rational Design of Gas Turbine Engine Compressor to Provide the Required Dynamic Strength Level of Rotor Blades

  • Daria Kolmakova, Grigorii Popov, Aleksandr Shklovets, Aleksandr Ermakov
  • June 2016, ASME International
  • DOI: 10.1115/gt2016-56991

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http://dx.doi.org/10.1115/gt2016-56991

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