THE problem of designing an aircraft so that the pilot is able easily to regain and maintain control following the sudden failure of an engine has been for some years a serious one. It is thought that an elementary description of the aerodynamics of the problem and of the flight tests which are made to assess a particular aircraft may be of interest. The equally important problem of ensuring adequate performance after an engine failure is not discussed here.


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    Titel :

    Control in Flight Under Asymmetric Power


    Untertitel :

    The Aerodynamics of the Problem of Regaining and Maintaining Control after Engine Failure


    Beteiligte:
    Yates, A.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.09.1947


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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