Results of investigation of large chord wing model with duct to house simulated radiator suitable for liquid cooled engine; duct was expanded to reduce radiator losses, and installation of duct and radiator was made entirely within wing to reduce form and interference drag.


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    Title :

    Investigation in 7- by 10-foot wind tunnel of ducts for cooling radiators within airplane wing


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Harris, T.A. (author) / Recant, I.G. (author)


    Publication date :

    1942


    Size :

    19 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





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