Airfoil has least amount of drag under given restrictions of boundary layer transition position, lift coefficient, thickness ratio, and Reynolds number based on airfoil chord. It is suitable for use as wing and propeller aircraft sections operating at subsonic speeds and for hydrofoil sections and blades for fans, compressors, turbines, and windmills.


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    Title :

    Design procedure for low-drag subsonic airfoils


    Contributors:

    Publication date :

    1975-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English