Apparatus and techniques developed or used by NASA-Lewis to make steady state or dynamic measurements of gas temperature, pressure, and velocity and of the temperature, tip clearance, and vibration of the blades of high-speed fans or turbines are described. The advantages and limitations of each instrument and technique are discussed and the possibility of modifying them for use in developing various propulsion systems is suggested.


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    Title :

    Instrumentation for propulsion systems development


    Contributors:

    Conference:

    Soc. of Automotive Engr. Congr. (Meeting 1M21) ; 1978 ; Detroit


    Publication date :

    1978-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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