The present report deals with a series of tests made for the purpose of improving flow conditions about wings by applying the suction principle (increase of the lift coefficient and reduction of the drag about very thick wing sections). Though not conclusive, the report contains interesting results.


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    Titel :

    Experiments with a Wing Model from which the Boundary Is Removed by Suction


    Beteiligte:
    Schrenk, Oskar (Autor:in)

    Erscheinungsdatum :

    1929-10-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Transition Flight Experiments on a Swept Wing With Suction

    Maddalon, D. V. / Collier, F. S., Jr. / Montoya, L. C. et al. | NTRS | 1989


    Transition Flight Experiments on a Swept Wing with Suction

    Maddalon, D. V. / Collier, F. S., Jr. / Montoya, L. C. et al. | NTRS | 1989