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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:

    Publication date :

    1994


    Size :

    19 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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

    Djatmiko, B. / Sudira, I. G. N. / Cakrawala, A. et al. | British Library Online Contents | 1994


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

    Djatmiko, B. / Sudira, I. G. N. / Cakrawala, A. et al. | British Library Conference Proceedings | 1994


    Effect of sweep on chevron slat noise

    Kopiev, Victor F. / Zaitsev, Mikhail / Belyaev, Ivan | AIAA | 2013


    An Analysis of Transonic Flow Around Double Sweep Back Wing

    Rho, O. / Kim, J. H. | British Library Conference Proceedings | 1993


    Wing slat actuator disconnection detection

    HUBBERSTEY MARK / TIMMS MARK | European Patent Office | 2020

    Free access