Advantages of conical head design over other kinds of thermometer head in high-speed flight; construction and wind tunnel tests; thermometer has remarkable constancy of recovery factor over range of Mach numbers from 0.2 to 0.9 and rapid response to temperature changes, lag coefficient being of order of 2 sec; possible extension of use of thermometer to supersonic flight.


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    Titel :

    Thermometer for high-speed aircraft


    Weitere Titelangaben:

    J Sci Instruments


    Beteiligte:
    Clark, D.D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1958


    Format / Umfang :

    7 pages



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Schlagwörter :


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