It is shown from elementary considerations that in zero incidence case lift coefficient and pressure distribution can be obtained directly (i.e. without solving flow problem fully) when jet momentum coefficient is small; formula is given.


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    Title :

    Some simple results for two-dimensional jet-flap aerofoils


    Additional title:

    Aeronautical Quarterly


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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