Mutual interference between rotors, wing, and tail of helicopter has large effect upon overall performance and stability of aircraft; equations are developed for all three induced velocity components at arbitrary point and for arbitrary harmonic of vorticity distribution.


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    Title :

    Equations for induced velocities near lifting rotor with nonuniform azimuthwise vorticity distribution


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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    Rotor Wake Computing With Lifting Lines and Vorticity Confinement

    Wenren, Y. / Steinhoff, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009