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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    Title :

    Thermometer for high-speed aircraft


    Additional title:

    J Sci Instruments


    Contributors:
    Clark, D.D. (author)

    Published in:

    Publication date :

    1958


    Size :

    7 pages



    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English


    Keywords :


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