Aerodynamic coefficients similar to those of the isolated airfoil are obtained as functions of the cascade geometry and the phasing between successive blades; the phasings considered are zero, 90 degrees, and 180 degrees. These aerodynamic coefficients are plotted for the special case when all the airfoils are vibrating in bending in phase (360 degree phasing). It is shown that the effect of cascading for this case is to reduce greatly the aerodynamic damping. (author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Lift and moment equations for oscillating airfoils in an infinite unstaggered cascade


    Beteiligte:

    Erscheinungsdatum :

    01.10.1954


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Lift and moment equations for oscillating airfoils in an infinite unstaggered cascade

    Mendelson, Alexander / Carroll, Robert W. | TIBKAT | 1954


    Lift Enhancement on Oscillating Airfoils

    Cleaver, David / Wang, Zhijin / Gursul, Ismet | AIAA | 2009


    Lift Enhancement on Oscillating Airfoils

    Cleaver, D. / Wang, Z. / Gursul, I. et al. | British Library Conference Proceedings | 2009


    High Lift, Low Pitching Moment Airfoils

    Noonan, Kevin W. | NTRS | 1988


    High-Lift, Low-Pitching-Moment Airfoils

    Noonan, Kevin W. | NTRS | 1987