3D Visualization of Unsteady 2D Airplane Wake Vortices

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 paper, we introduce three-dimensional techniques for visualizing time-dependent, two-dimensional wake vortex 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 calculates 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. We also suggest ways of combining multiple visualization methods to present more information simultaneously.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1994
Accession Number
ADA284745

Entities

People

  • Kwan-liu Ma
  • Z. C. Zheng

Tags

Communities of Interest

  • Air Platforms
  • Biomedical
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Algorithms
  • Boundaries
  • Boundary Layer
  • Differential Equations
  • Engineering
  • Equations
  • Flow Fields
  • Flow Visualization
  • Layers
  • Partial Differential Equations
  • Poisson Equation
  • Simulations
  • Stratified Fluids
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aviation Safety and Air Traffic Management
  • Computational Modeling and Simulation
  • Fluid Mechanics and Fluid Dynamics.