Account of tests made in NACA free spinning tunnel to determine effect of systematic changes in wing and tail arrangements upon steady spinning and recovery characteristics of conventional low wing monoplane model for basic loading conditions.


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    Title :

    Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails, I -- Basic loading condition


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:


    Publication date :

    1937


    Size :

    13 pages


    Remarks:

    17 Supp plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English