Study to determine effects of adding stiffener frames, frame height and spacing, and scale on aerodynamic heating characteristics of skin in missile wall; three flat plate models simulating various stiffening arrangements and one with no stiffeners were tested in 27-×27-in. nozzles of preflight jet of Langley Pilotless Aircraft Research Station; addition of stiffeners caused large pressure losses in flow along plate.


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    Title :

    Effect of some external crosswise stiffeners on heat transfer and pressure distribution on flat plate at Mach numbers of 0.77, 1.39, and 1.98


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1958


    Size :

    21 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :