An analysis of the lift augmentation due to a thin jet of air issuing from a slot along the leading edge of a delta wing is presented. The problem is treated with an extension of the method of Brown and Michael, representing the separated flow on the lee side of the wing by a pair of concentrated vortices and corresponding feeding sheets. It is assumed that the jet is not affected by Coanda forces. The analysis produces qualitative agreement with experiments.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    The lift of sharp-leading-edged delta wings with blowing


    Beteiligte:
    Tavella, D. A. (Autor:in)

    Erscheinungsdatum :

    01.12.1985


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Flow Control of Sharp-Edged Wings via Unsteady Blowing

    Rullan, J. / Vlachos, P. P. / Telionis, D. P. et al. | British Library Conference Proceedings | 2004


    Post-Stall Flow Control of Sharp-Edged Wings via Unsteady Blowing

    Jose Rullan / Pavlos Vlachos / Demetri Telionis et al. | AIAA | 2006


    Post-Stall Flow Control of Sharp-Edged Wings via Unsteady Blowing

    Rullan, Jose / Vlachos, Pavlos / Telionis, Demetri et al. | AIAA | 2004


    Post-Stall Flow Control of Sharp-Edged Wings via Unsteady Blowing

    Rullan, J. / Vlachos, P. P. / Telionis, D. P. et al. | British Library Conference Proceedings | 2003