A thick delta wing with a rounded leading egde has been experimentally studied. To understand the basic flow field of such a wing, experiments have been conducted in low speed wind tunnel at Nagoya university. Three types of flow visualization: oil flow, smoke wire, and tuft methods are employed, and forces: lift and drag, and pressure distributions were also obtained. The same test has been conducted for a thin delta wing for comparison.The results show the different flow field of the thick delta wing from those commonly known for delta wings. However, in other properties except for the flow pattern, similarities were observed between the thick delta wing and thin delta wing.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Flow Field Around Thick Delta Wing with Rounded Leading Edge


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    International Pacific Air & Space Technolgy Conference ; 1991



    Erscheinungsdatum :

    1991-09-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Control of Vortical Flow over a Rounded Leading-Edge Delta Wing

    Florent Renac / Didier Barberis / Pascal Molton | AIAA | 2005


    Control of vortical flow over a rounded leading-edge delta wing

    Renac, Florent / Barberis, Didier / Molton, Pascal | Tema Archiv | 2005



    Control of vortical flows over a rounded leading-edge delta wing

    Renac, Florent / Barberis, Didier / Molton, Pascal | AIAA | 2003