Incremental pressure distributions due to spoilers were in good agreement with previous flat plate results and tests of spoilers on trapezoidal wing; spanwise loadings and integrated lift, bending and pitching moment coefficients presented.


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    Title :

    Pressure distributions and aerodynamic characteristics of several spoiler controls on 40° sweptback wing at mach number of 1.61


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    66 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :