Flight tests revealed excessive vibration in cabin; source of vibration was aerodynamic in nature, specifically, interference condition between propeller slipstream and stabilizer; surveys of flow at tail indicated that at cruising engine speeds, in level flight, slipstream just bordered on horizontal stabilizer and created vibration in tail unit which was transmitted into fuselage; changes made. Before Inst Aeronautical Sciences.


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    Titel :

    Effects of propeller slipstream and tail position on vibration characteristics of lockheed lodestar


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Thoren, R.L. (Autor:in) / Johnson, C.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1940


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Lockheed lodestar

    Engineering Index Backfile | 1941



    Propeller Slipstream Development

    Roosenboom, E. / Heider, A. / Schroder, A. et al. | British Library Conference Proceedings | 2007


    Propeller Slipstream Development

    Roosenboom, Eric / Heider, André / Schröder, Andreas | AIAA | 2007