Tests are part of general investigation being made in NACA free spinning tunnel to determine effect of systematic changes in wing and tail arrangement upon steady spinning and recovery characteristics of conventional low wing monoplane for various loading conditions.


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    Title :

    Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails, II mass distributed along fuselage, III. mass distributed along wings


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1937


    Size :

    11 pages


    Remarks:

    17 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :