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Information × Registration Number 0211U005719, 0111U001847 , R & D reports Title Development of the integrated experimental-computational system to predict the stability of blade assemblies against subsonic flutter popup.stage_title Head Zinkovskii Anatoly P., Registration Date 23-12-2011 Organization Institute for problems of strength NASci of Ukraine popup.description2 An integrated experimental-computational system to predict the stability of aircraft gas turbine engine blading against subsonic flutter has been developed, its scientific-and-technical justification has been carried out and the results of its testing have been presented using as an example the estimation of the stability boundary of modern gas turbine engine compressor blading against subsonic cascade flutter Product Description popup.authors Зіньковський Анатолій Павлович Цимбалюк Володимир Анатолійович popup.nrat_date 2020-04-02 Close