The interrelations established in an earlier report (NACA-TM-921) are used to study the best assumptions for hovering and horizontal flight. The effect of the twisted and tapered blade on the rotor efficiency is analyzed and the gliding coefficient at different stages (from autogyro to helicopter) of horizontal flight compared. To the extent that model or full-scale test data are available, they are included in the comparison.


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    Titel :

    Contribution to the aerodynamics of rotating-wing aircraft. Part II


    Beteiligte:
    Sissingh, G (Autor:in)

    Erscheinungsdatum :

    1941-10-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Contribution to aerodynamics of rotating wing aircraft

    Sissingh, G. | Engineering Index Backfile | 1941


    Aerodynamics of rotating-wing aircraft with bladepitch control

    Pflueger, A. | Engineering Index Backfile | 1940