This paper discusses the results of a cooperative experimental research program on a half-model of a fuselage and wing with high lift devices (slat and flap) equipped with zero and 25 deg sweep capability. Tests were made with two wing seeps, 0 and 25 deg. The results include: Basic forces and surface pressure distributions; Three-dimensional confluent boundary layer measurements at two spanwise and three chordwise stations on the main wing; Total pressure measurements at the slat cove; and Surface flow visualizations.


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    Titel :

    Effect of Wing Sweep on the Flow Around a Slat and Its Performance


    Beteiligte:
    B. Djatmiko (Autor:in) / I. G. N. Sudira (Autor:in) / A. Cakrawala (Autor:in) / B. van den Berg (Autor:in) / S. H. Chintamani (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    19 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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