Temperature measurements made in skin of wing, tested on model propelled by 2-stage rocket propulsion system, agreed well with calculated values; measured values of Stanton number were in reasonably good agreement with theory of Van Driest for flat plates with turbulent boundary layers.


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    Titel :

    Free-flight investigation of rocket-propelled model to determine aerodynamic heating on thin, unswept, untapered, multispar aluminum-alloy wing at mach numbers up to 2.22


    Weitere Titelangaben:

    NASA -- Memo


    Beteiligte:
    Stephens, E.W. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    38 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :