This report discusses in detail the results obtained with devices for preventing the separation of the boundary layer. In order to give an idea of the order of magnitude of the positive and negative pressures involved, we made a diagram of them, as measured at 15 degrees angle of attack on the Gottigen profile 387. The pressure scale is graduated in terms of the dynamic pressure q, which enables the evaluation of the positive and negative pressures at all velocities.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    The use of slots for increasing the lift of airplane wings


    Contributors:
    Haus, FR (author)

    Publication date :

    1931-08-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



    Use of slots for increasing lift of airplane wings

    Haus, F. | Engineering Index Backfile | 1931


    Use of slots for increasing lift of airplane wings

    Haus, F. | Engineering Index Backfile | 1931



    Simple method for increasing lift of airplane wings by means of flaps

    Gruschwitz, E. / Schrenk, O. | Engineering Index Backfile | 1933


    Application of slots and flaps to airplane wings in America

    Wright, T.P. | Engineering Index Backfile | 1933