Instrument in form of fuselage nose containing pitot and static orifices for measuring pressure altitude and indicated air speed, and vane transducers for measuring angle of attack and angle of sideslip.


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    Title :

    Aircraft instrument boom design


    Additional title:

    Aero Digest


    Contributors:

    Published in:

    Aero Digest ; 68 , n 1


    Publication date :

    1954


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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