A combined computational/experimental investigation has been conducted to determine the time-averaged interactive performance of a propeller and wing in tractor configuration at Mach 0.1 and Re=470,000, based on a wind tunnel model wing chord of 8 in. Wing angle-of-attack was varied from 0 to +13 deg, and propeller advance ratio ranged from 2.4 (windmilling) to 1.1 (maximum power). Both a semiempirical model and a vortex lattice simulation were used in the computational analysis. Good agreement has been obtained between theory and experiment.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic interaction between propellers and wings


    Beteiligte:

    Erscheinungsdatum :

    01.01.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic interaction between propellers and wings

    WITKOWSKI, DAVE P. / LEE, ALEX K. H. / SULLAN, JOHN P. | AIAA | 1989


    Aerodynamic interaction between propellers and wings

    Witkowski, Dave P. / Lee, Alex K. H. / Sullivan, John P. | NTRS | 1989


    Aerodynamic interaction between propellers and wings

    WITKOWSKI, DAVID / LEE, ALEX / SULLIVAN, JOHN | AIAA | 1988


    Aerodynamic Interaction Effects Between Propellers in Typical eVTOL Vehicle Configurations

    Stokkermans, Tom C. A. / Usai, Daniele / Sinnige, Tomas et al. | AIAA | 2021