On helicopter in forward flight, inboard blade elements that pass through reverse flow region experience change in angle of attack of 360° once each revolution; in other flight conditions, angles of attack of fairly large areas of blades are beyond usual values for which data are customarily presented; program carried out to make available data for representative airfoil in unfamiliar range, at Reynolds Number close to flight conditions.


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    Title :

    Forces and moments over NACA 0015 airfoil through 180° angle of attack


    Additional title:

    Aero Digest


    Contributors:
    Pope, A. (author)

    Published in:

    Aero Digest ; 58 , n 4


    Publication date :

    1949


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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