No. 522; Concluding paper on investigation of landing-gear drag carried out in N.A.C.A. 20-ft wind tunnel; tests of tail wheels and tail skids; drag of landing gear, for which interference between wheels and struts is small, is appreciably less with streamline wheels than with low-pressure wheels of equal load-carrying capacity. (Price 10¢) (See also - report n 518 1935 10 p. 10¢)


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    Title :

    Drag of airplane wheels, wheel fairings and landing gears. II -- Nonretractable and partly retractable landing gears


    Additional title:

    Nat. Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1935


    Size :

    11 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English