The tests reported in this report conclude the investigation of landing-gear drag that has been carried out in the NACA 20-foot wind tunnel. They supplement earlier tests (reported in Technical Report No. 485) made with full-scale dummy wheels, wheel fairings, and landing gears intended for airplanes of 3,000 pounds gross weight and include tests of tail wheels and tail skids.


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    Title :

    The Drag of Airplane Wheels, Wheel Fairings, and Landing Gears - III


    Contributors:

    Publication date :

    1936-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



    Drag of airplane wheels, wheel fairings, and landing gears

    Herrnstein, Jr., W.H. / Biermann, D. | Engineering Index Backfile | 1934


    Drag of Airplane Wheels, Wheel Fairings and Landing Gears-I

    W. H. Herrnstein / D. Biermann | NTIS | 1934


    The Drag of Airplane Wheels, Wheel Fairings, and Landing Gears - I

    Herrnstein, William H / Biermann, David | NTRS | 1935