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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    Title :

    Control in Flight Under Asymmetric Power


    Subtitle :

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


    Contributors:
    Yates, A.H. (author)

    Published in:

    Publication date :

    1947-09-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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