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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    Title :

    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


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1959


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :