New tested method of airfoil selection is conceived to assist in overcoming present hazardous stalling tendencies on highly tapered (3:1 or more) and swept back (15° or more) wings, and to control stall at inception and through progression; method eliminates high drag penalties and other undesirable characteristics that develop with washout and highly cambered wing tips when employing two controlled sections.


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    Title :

    Effective control of stalling characteristics of highly tapered and swept-back wings


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1946


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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