Device developed by Boulton Paul Aircraft Ltd, undergoing trials on "Lancaster" aircraft; in system electromanometric transducer mounted at nose of aircraft detects vertical components of gust pressures which require symmetrical displacements of ailerons if level flight is to be maintained.


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    Titel :

    Gust alleviation device for aircraft


    Weitere Titelangaben:

    Engineer


    Erschienen in:

    Engineer ; 192 , n 4980


    Erscheinungsdatum :

    1951


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Gust alleviation for STOL aircraft

    Oehman, W. I. | NTRS | 1976


    Gust Alleviation for General Aviation Aircraft

    Kimberlin, R. D. / Sims, J. P. / SAE et al. | British Library Conference Proceedings | 1996


    Gust Alleviation for General Aviation Aircraft

    Sims, J. Paul / Kimberlin, Ralph D. | SAE Technical Papers | 1996


    Gust alleviation

    Phillips, W. H. | NTRS | 1971


    PASSIVE GUST ALLEVIATION SYSTEMS FOR AIRCRAFT DEVICES

    DECKER GEORGE R | Europäisches Patentamt | 2020

    Freier Zugriff