Improved probe designed to be mounted at wingtip of airplane and used for measuring total temperature of air when airplane flies at high angles of attack. Four fins and swivel mount enable probe to align itself aerodynamically with local flow of air. Thus, stagnated-flow condition needed for accurate measurement of total temperature achieved.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Swivel Total-Temperature Probe


    Contributors:
    Moes, Tim (author) / Nichols, Doug (author) / Vanderloop, Dirk (author) / Rood, Rich (author)

    Published in:

    Publication date :

    1996-03-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Swivel Total-Temperature Probe

    Online Contents | 1996


    Swivel

    MUPENDE ILAKA DR / ZERZA HORST | European Patent Office | 2018

    Free access

    SWIVEL

    SÄRNDAHL ALBIN | European Patent Office | 2016

    Free access

    SWIVEL

    ALFSEN FRODE / NYGÅRD STIG ANDRÉ KITTELSEN / TØNNESSEN JON | European Patent Office | 2023

    Free access

    SWIVEL

    MUPENDE ILAKA / ZERZA HORST | European Patent Office | 2016

    Free access