Investigations to obtain information which would lead to design of rigid type tubes capable of measuring total pressures correctly at high angles of attack and at high speeds.


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    Title :

    Wind-tunnel investigation of number of total-pressure tubes at high angles of attack -- Subsonic, transonic, and supersonic speeds


    Additional title:

    NACA -- Tech Note


    Contributors:
    Gracey, W. (author)


    Publication date :

    1956


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English