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 Aeronautical Eng Rev v 9 n 6 June 1950 p 22-7)


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    Title :

    Practical instrument flying in helicopter


    Additional title:

    Aero Digest


    Contributors:

    Published in:

    Aero Digest ; 61 , n 2


    Publication date :

    1950


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Practical instrument flying in helicopter

    Cannon, J.A. / Niehaus, O.Q. | Engineering Index Backfile | 1950


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    Green, D. L. / Kimberlin, R. D. / Society of Automotive Engineers | British Library Conference Proceedings | 1994


    Helicopter Unique Instrument Approaches: Trajectories, Flying Qualities, Controls and Displays

    Green, David L. / Kimberlin, Ralph D. | SAE Technical Papers | 1994


    Flying in mil helicopter

    Fricker, J. | Engineering Index Backfile | 1956


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

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