3D visualization of unsteady 2D airplane wake vortices

  • Authors:
  • Kwan-Liu Ma;Z. C. Zheng

  • Affiliations:
  • NASA Langley Research Center, Hampton, Virginia;Old Dominion University, Norfolk, Virginia

  • Venue:
  • VIS '94 Proceedings of the conference on Visualization '94
  • Year:
  • 1994

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Abstract

Air flowing around the wing tips of an airplane forms horizontal tornado-like vortices that can be dangerous to following aircraft. The dynamics of such vortices, including ground and atmospheric effects, can be predicted by numerical simulation, allowing the safety and capacity of airports to be improved. In this payer, we introduce three-dimensional techniques for visualizing time-dependent, two-dimensional wake vorte computations, and the hazard strength of such vortices near the ground. We describe a vortex core tracing algorithm and a local tiling method to visualize the vortex evolution. The tiling method converts time-dependent, two-dimensional vortex cores into three-dimensional vortex tubes. Finally, a novel approach is used to calculate the induced rolling moment on the following airplane at each grid point within a region near the vortex tubes and thus allows three-dimensional visualization of the hazard strength of the vortices.