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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    Titel :

    Practical instrument flying in helicopter


    Weitere Titelangaben:

    Aeronautical Eng Rev


    Beteiligte:
    Cannon, J.A. (Autor:in) / Niehaus, O.Q. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1950


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Practical instrument flying in helicopter

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


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

    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


    Defence Helicopter Flying School

    Online Contents | 1997