Existing data on measurement by means of static pressure tubes and fuselage vents at subsonic, transonic, and supersonic speeds, presented; static pressure errors for isolated tubes and vents, installations ahead of fuselage nose, wing tip, and vertical tail fin, and fuselage; methods of calibrating installations in flight. See also Engineering Index 1951 p 13, under Aeronautical Instruments -- Air Speed Indicators.


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    Title :

    Measurement of static pressure on aircraft


    Additional title:

    NACA -- Tech Note


    Contributors:
    Gracey, W. (author)


    Publication date :

    1957


    Size :

    71 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Measurement of static pressure on aircraft

    Gracey, William | NTRS | 1958


    Measurement of static pressure on aircraft

    Gracey, William | SLUB | 1959


    Measurement of Static Pressure on Aircraft

    Gracey, William | NTRS | 1957


    Measurement of static pressure on aircraft

    Gracey, William | TIBKAT | 1957


    Measurement of static pressure on aircraft

    Gracey, William | NTRS | 1957