Tests made in atmospheric wind tunnel of Nat. Advisory Comm. for Aeronautics to determine effects of pitching oscillations upon lift of airfoil; it has been found that lift of airfoil, while pitching, is usually less than that which would exist at same angle of attack in stationary condition, and that behavior of pitching airfoil may be qualitatively explained on basis of accepted aerodynamic theory.


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    Title :

    Airfoil lift with changing angle of attack


    Additional title:

    Nat. Advisory Comm. Aeronautics -- Tech. Note


    Contributors:
    Reid, E.G. (author)


    Publication date :

    1927


    Size :

    15 pages


    Remarks:

    9 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Airfoil Lift with Changing Angle of Attack

    Reid, Elliott G | NTRS | 1927


    Airfoil lift with changing angle of attack

    Reid, Elliott G. | SLUB | 1927


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