Two models were tested, one with symmetrical airfoil sections and other with same basic thickness forms but with reflex cambered mean line.


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    Title :

    Effect of reflex chamber on aerodynamic characteristics of highly tapered moderately swept-back wing at Reynolds numbers up to 8,000,000


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    10 pages


    Remarks:

    13 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :