A high rim speed turbine incorporating 3-D features is designed and tested. The cold flow turbine testing, with performance measurements, rotor exit traversing and surface static pressure measurements on the vane and rotor, is performed. The vane is tested in annular cascade on the isentropic light piston cascade. Surface heat transfer measurements on the vanes and endwalls and aerodynamic information are given. The data is compared with design predictions and the reasons for the differences observed are explored.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic and Heat Transfer Measurements on Blading for a High RIM-Speed Transonic Turbine


    Beteiligte:
    R. C. Kingcombe (Autor:in) / S. P. Harasgama (Autor:in) / N. P. Leversuch (Autor:in) / E. T. Wedlake (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Turbine blading problems

    Robinson, S.M. | Engineering Index Backfile | 1928


    Turbine blading designed for high heat load space propulsion applications

    CINSKAS, K. C. / BOYLE, R. J. / MCCONNAUGHEY, H. V. | AIAA | 1990


    Turbine blading designed for high heat load space propulsion applications

    Civinskas, K. C. / Boyle, R. J. / Mcconnaughey, H. V. | NTRS | 1990


    FEATURES OF AERODYNAMIC AND HEAT TRANSFER MEASUREMENTS FOR A FULLY-COOLED SINGLE STAGE HP TRANSONIC TURBINE STAGE

    Dunn, M. / Haldeman, C. / International Society for Air Breathing Engines | British Library Conference Proceedings | 2009