A Flow Visualisation Study to Tip Vortex Formation,

Abstract

The process by which a wing or rotor blade tip vortex is generated has been studied in a water tunnel using dye and hydrogen bubble flow visualisation techniques. In particular, the effects of the shape of the lateral tip edge on vortex formation have been examined. Three edges shapes were tested-a square tip, a square tip with rounded fairing, and a square tip with bevelled fairing. The square tip was found to have the most complicated vortex system, with vortices forming on the tip edge face as well as above the wing. The observed flow features ere generally similar to those proposed in the literature on the basis of pressure measurements, velocity measurements, and surface flow visualization in wind tunnels and on whirl towers. The vortex systems for the rounded and bevelled tips were less complicated. The shape of the tip edge has a significant effect on the structure of the tip vortex system, and may thus influence the tip loading characteristics. Verification of this will require further testing. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1983
Accession Number
ADA142846

Entities

People

  • D. H. Thompson

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircraft Wings
  • Aircrafts
  • Airframes
  • Argon Lasers
  • Boundary Layer
  • Flow Visualization
  • Fluid Mechanics
  • Measurement
  • Mechanical Engineering
  • Pressure Distribution
  • Pressure Measurement
  • Reynolds Number
  • Stratified Fluids
  • Test Facilities
  • Water Tunnels
  • Wind Tunnels
  • Wing Tips

Readers

  • Aerodynamics.
  • Fluid Mechanics and Fluid Dynamics.