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
Link To Document :
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