Use of Liquid Crystals for Qualitative and Quantitative 2-D Studies of Transition and Skin Friction

Abstract

The exploitation of the properties of liquid crystals for use in wind tunnels to visualize transition and to measure skin friction is described. The effectiveness of a transition band to trip the laminar boundary layer on a swept wing is demonstrated by the growth of turbulent wedges with Reynolds number. The ability to liquid crystals to reveal intricate surface flow structure is clearly shown by subtle changes of colour on an unswept rectangular wing when subjected to the combined effects of transition, separation, reattachment and a normal shock. The time response of liquid crystals to changes in shear stress is illustrated by the shock pattern on the model surface which was seen to be oscillating. A method involving the digitisation of the video image into its three component colours has the potential for measuring skin friction in great detail. This involves using relationships firstly correlating the component colours with wavelength and secondly correlating shear stress with wavelength. Great Britain.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1989
Accession Number
ADA218227

Entities

People

  • L. Gaudet
  • T. G. Gell

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundary Layer
  • Cameras
  • Climate Change
  • Flow Visualization
  • Friction
  • Leading Edges
  • Liquid Crystals
  • Mach Number
  • Measurement
  • Reynolds Number
  • Shear Stresses
  • Skin Friction
  • Surface Temperature
  • Swept Wings
  • Two Dimensional
  • Wind Tunnel Models
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design
  • Thermal Physics or Thermal Science.