Force tests on and airflow surveys near autogiro rotor in NACA full-scale wind tunnel; force tests made at three pitch settings and several rotor speeds; effect of fairing protuberances on rotor blade; induced downwash and yaw angles at two tip-speed ratios in plane 1 1/2 ft above path of blade tips. (Price 5¢)


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    Title :

    Full-scale wind-tunnel tests of PCA-2 autogiro rotor


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Wheatley, J.B. (author) / Hood, M.J. (author)


    Publication date :

    1935


    Size :

    10 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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