Elementary description of aerodynamics of problem of regaining and maintaining control after engine failure; three situations considered are: sudden failure of engine; steady flight under asymmetric power; balked landing with one or more engines dead.


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    Title :

    Control in flight under asymmetric power


    Additional title:

    Aircraft Eng


    Contributors:
    Yates, A.H. (author)

    Published in:

    Aircraft Engineering ; 19 , n 223 ; p 287-290


    Publication date :

    1947


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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