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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    Titel :

    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


    Weitere Titelangaben:

    NACA -- Tech Note


    Beteiligte:
    Carter, H.S. (Autor:in)


    Erscheinungsdatum :

    1958


    Format / Umfang :

    21 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :