Tests were made to determine some effects of chordwise location for spoilers and blowing direction and spanwise location for jets; all controls were satisfactory roll-producing devices except canards immediately forward of main wings and spoilers at other than trailing-edge locations.


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    Title :

    Free-flight investigation at mach numbers between 0.5 and 1.7 of zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on 80° delta-wing missile


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    47 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :