Abstract Some results of investigating the geometrical and jet impact on secondary flows and thermal state of cooled inter-profile end surfaces of gas turbine engine nozzles have been set forth under different secondary flows interaction degree in a blade channel.


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    Titel :

    Special features of aerodynamic and thermal improvement of turbine nozzles for advanced gas turbine engines


    Beteiligte:
    Poletaev, V. A. (Autor:in) / Remizov, A. E. (Autor:in) / Vyatkov, V. V. (Autor:in) / Lebedev, V. V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2016-01-01


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Special features of aerodynamic and thermal improvement of turbine nozzles for advanced gas turbine engines

    Poletaev, V. A. / Remizov, A. E. / Vyatkov, V. V. et al. | Online Contents | 2016


    Turbine nozzles and diaphragms

    Scorer, S.D. | Engineering Index Backfile | 1933



    Turbine pyrometry for advanced engines

    ATKINSON, W. | AIAA | 1987