Investigation carried out in test blower; performance of four sets of rotor blades, designed to set up free vortex flow and operating with design pitch-section lift coefficients from 0.31 to 0.99, was studied by making surveys of yaw angles and pressures; tests made in single-stage test blower at Langley Memorial Aeronautical Laboratory of NACA.


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    Titel :

    Performance of axial-flow fan and compressor blades designed for high loadings


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Bogdonoff, S.M. (Autor:in) / Herrig, L.J. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    13 pages


    Anmerkungen:

    18 Supp Plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :