Pressure-distribution diagrams, as well as integrated characteristics of airfoils, are given for both high and low dynamic scale Reynolds Number VI/v for comparison with flight and other wind tunnel tests respectively; development of approximate method of predicting pressure distribution along chord of any normal airfoil.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Airfoil pressure distribution investigation in the variable density wind tunnel


    Additional title:

    Nat. Advisory Committe Aeronautics -- Report


    Contributors:
    Jacobs, E.N. (author) / Stack, J. (author) / Pinkerton, R.M. (author)


    Publication date :

    1930


    Size :

    16 pages


    Remarks:

    12 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :