It has been identified that vorticity in a vortex core directly relates to the frequency of a significant sound peak from an aircraft wake vortex pair where each of the vortices is modeled as an elliptic core Kirchhoff vortex. In three-dimensional vortices, sinusoidal instabilities at various length scales result in significant flow structure changes in these vortices, and thus influence their radiated acoustic signals. In this study, a three-dimensional vortex particle method is used to simulate the incompressible vortical flow. The flow field, in the form of vorticity, is employed as the source in the far-field acoustic calculation using a vortex sound formula that enables computation of acoustic signals radiated from an approximated incompressible flow field. Cases of vortex rings and a pair of counter-rotating vortices are studied when they are undergoing both long- and short-wave instabilities. Both inviscid and viscous interactions are considered and effects of turbulence are simulated using sub-grid-scale models.
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ASME 2007 International Mechanical Engineering Congress and Exposition
November 11–15, 2007
Seattle, Washington, USA
Conference Sponsors:
- ASME
ISBN:
0-7918-4295-9
PROCEEDINGS PAPER
Flow/Acoustic Mechanisms in Three-Dimensional Vortices Undergoing Sinusoidal-Wave Instabilities
Wenhua Li,
Wenhua Li
Kansas State University, Manhattan, KS
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Z. C. Zheng,
Z. C. Zheng
Kansas State University, Manhattan, KS
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Ying Xu
Ying Xu
Kansas State University, Manhattan, KS
Search for other works by this author on:
Wenhua Li
Kansas State University, Manhattan, KS
Z. C. Zheng
Kansas State University, Manhattan, KS
Ying Xu
Kansas State University, Manhattan, KS
Paper No:
IMECE2007-43163, pp. 101-120; 20 pages
Published Online:
May 22, 2009
Citation
Li, W, Zheng, ZC, & Xu, Y. "Flow/Acoustic Mechanisms in Three-Dimensional Vortices Undergoing Sinusoidal-Wave Instabilities." Proceedings of the ASME 2007 International Mechanical Engineering Congress and Exposition. Volume 1: Advances in Aerospace Technology. Seattle, Washington, USA. November 11–15, 2007. pp. 101-120. ASME. https://doi.org/10.1115/IMECE2007-43163
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