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)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Practical instrument flying in helicopter


    Weitere Titelangaben:

    Aero Digest


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

    Erschienen in:

    Aero Digest ; 61 , n 2


    Erscheinungsdatum :

    1950


    Format / Umfang :

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


    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


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

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


    Flying Helicopter EGPWS

    Aarons, R. N. | British Library Online Contents | 2001