Wind tunnel results are corrected for model or airfoil by measurements of lift, etc, with and without dummy supports fitted; it is useful to have some independent check by direct calculation on amount of interference to be expected; theory for rectangular airfoil.


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    Title :

    Strut interference on aerofoil


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1956


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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