Aerodynamic force tests of a Clark Y wing equipped with "Maxwell" type leading-edge slots were conducted in the N.A.C.A. 7- by 10-foot tunnel to ascertain the aerodynamic characteristics, which involved the determination of the best slot-gap opening, the effects of slat width, and the effect of a trailing-edge flap. The Maxwell wing with a wide-chord slat (0.30 c(sub w)) and with a 0.211 c(sub w) split flap deflected 60 degrees had a C(sub L sub max) of 2.53 or about twice that of the plain wing. The wing with the wide slat also had, in general, improved aerodynamic characteristics over those of the Maxwell wing with slat, and had about the same aerodynamic characteristics as a Handley Page slotted wing with approximately the same size of slat.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Wind-tunnel tests of a Clark Y wing with 'Maxwell' leading-edge slots


    Beteiligte:

    Erscheinungsdatum :

    01.04.1937


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Wind-tunnel tests of Clark Y wing with "maxwell" leading-edge slots

    Gauvain, W.E. | Engineering Index Backfile | 1937




    Wind-tunnel tests of clark Y wing having split flaps with gaps

    Wenzinger, C.J. | Engineering Index Backfile | 1938


    Wind-tunnel tests of clark Y wing having split flaps with gaps

    Wenzinger, C.J. | Engineering Index Backfile | 1938