Practical flight test had as its primary objective determination of instrumentation requirements needed for satisfactory instrument flight within 40 mph to Vmax air speed range; instrument flying at very low speed with emphasis on 0-15 mph range. (see also Aero Digest v 61 n 2 Aug 1950 p 24, 26, 28, 100-2)


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    Title :

    Practical instrument flying in helicopter


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1950


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Practical instrument flying in helicopter

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    Initial results of instrument-flying trials conducted in single-rotor helicopter

    Crim, A.D. / Reeder, J.P. / Whitten, J.B. | Engineering Index Backfile | 1952