• DocumentCode
    2662911
  • Title

    Notice of Retraction
    Vortex breakdown over delta wing and its induced turbulent flow

  • Author

    Dang Huixue ; Yang Zhichun

  • Author_Institution
    Sch. of Aeronaut., Northwestern Polytech. Univ., Xi´an, China
  • Volume
    5
  • fYear
    2010
  • fDate
    16-18 April 2010
  • Abstract
    Notice of Retraction

    After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.

    We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.

    The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.

    Vortex breakdown over delta wing is simulated by solving Navier-Stokes equations. Iso-surfaces of total pressure and flow parameters along vortex core axis are employed to depict this phenomena. To have an insight into the turbulence characteristics induced by vortex breakdown, iso-surfaces of turbulent kinetic energy and turbulence dissipation rate are employed. The results indicated that, vortex breakdown location moves upstream with the increase of incidence angle. During vortex breakdown process, kinetic energy of leading edge vortex is transformed into kinetic energy of small vortices and turbulent kinetic energy. Turbulent kinetic energy of vortex breakdown wake is also fed by energy transformation from small vortices. At the same time, turbulent kinetic energy is dissipated by inner shear friction during the evolutions of leading edge vortex and vortex breakdown wake. The feeding and dissipation of kinetic energy together govern the dissipation process of vortex breakdown. Complex interferences include mutual-inductions in between small vortices and self-induction of single vortex, causing stretching, compression, wandering and distortion of these vortices, and this is the reason for highly unsteady flow in vortex breakdown wake.
  • Keywords
    Navier-Stokes equations; aerospace components; friction; turbulence; vortices; Navier-Stokes equations; aircraft; delta wing; induced turbulent flow; shear friction; turbulence dissipation; turbulent kinetic energy; vortex breakdown; Electric breakdown; Friction; Interference; Kinetic energy; Military aircraft; Navier-Stokes equations; Numerical simulation; Performance loss; Spirals; Testing; delta wing; induction; turbulent kinetic energy; unsteady; vortex breakdown;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Engineering and Technology (ICCET), 2010 2nd International Conference on
  • Conference_Location
    Chengdu
  • Print_ISBN
    978-1-4244-6347-3
  • Type

    conf

  • DOI
    10.1109/ICCET.2010.5486142
  • Filename
    5486142