Low speed investigation in Langley stability tunnel showed that these effects were important factors in directional stability characteristics of fuselage-tail configuration; study of air flow behind fuselage model by tuft grid technique.


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    Title :

    Wind-tunnel investigation of effects of spoiler location, spoiler size, and fuselage nose shape on directional characteristics of model of tandem-rotor helicopter fuselage


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1958


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :