Flight investigation was made with sweptback wing aircraft fighter and wind tunnel investigation on semispan wing model in Langley 300-mph 7- by 10-ft tunnel; results on rolling effectiveness and hinge-moment characteristics of paddle spoilers at various subsonic speeds.


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    Title :

    Limited flight and wind-tunnel investigation of paddle spoilers as lateral controls


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :