The overall and blade-element performance of a low pressure ratio, low tip speed fan stage at design speed is presented for tow off-design rotor blade angle settings. The rotor design tip speed is 243.8 m/sec and weight flow per unit annulus area is 175.8 kg/sec. Design weight flow and pressure ratio are 29.9 kg/sec and 1.151, respectively.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Performance of Low-Pressure-Ratio Fan Stage at Two off-Design Blade Setting Angles


    Beteiligte:
    G. Kovich (Autor:in) / E. R. Tysl (Autor:in) / R. D. Moore (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    90 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Performance of low-pressure-ratio fan stage at two off-design blade setting angles

    Kovich, George / Tysl, Edward R. / Moore, Royce D. | TIBKAT | 1977





    Investigations on A High Pressure Ratio Centrifugal Compressor with Highly Backward-Swept Blade Angles

    Choi, J. H. / Sung, O. S. / Chen, S.-B. et al. | British Library Conference Proceedings | 2005