Study to extend range of calibration Mach numbers and to assess effects of presence of temperature element; error curves for pitot-static pressure measurements and flow direction vane correction curves for range of angles of attack and sideslip are presented.


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    Title :

    Wind-tunnel calibrations of combined pitot-static tube, vane-type flow-direction transmitter, and stagnation-temperature element at Mach numbers from 0.60 to 2.87


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English