In support of theoretical methods presented, experimental data have been secured on various pressure systems in frequency range up to 70 cycles per sec; both frequency range and pressure systems tested were chosen as being representative of conditions which would be encountered in flight and wind tunnel installations.


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    Title :

    Response of pressure measuring systems to oscillating pressures


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Taback, I. (author)


    Publication date :

    1949


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English