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Photon Correlation Velocimetry in Aerodynamics

  • J. B. Abbiss
Part of the Nato Advanced Study Institutes Series book series (NSSB, volume 23)

Abstract

For the aerodynamicist, the attraction of laser-Doppler measurement techniques is that they are essentially non-intrusive; they do not disturb the flow being studied. This is of particular value in certain classes of fluid-mechanical problem, where conventional instruments, such as hot-wire probes and pitot tubes, have serious limitations: for example, in recirculating and separated flows, in conditions of high turbulence, in the investigation of jet noise and in the study of vortex evolution. A research topic of practical importance for supercritical wing design is the detailed structure of the interaction between a normal shock wave and a turbulent boundary layer. Here, as we shall see, the laser anemometer has already yielded fundamentally new information.

Keywords

Mach Number Autocorrelation Function Turbulence Intensity Turbulent Boundary Layer Supersonic Flow 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer Science+Business Media New York 1977

Authors and Affiliations

  • J. B. Abbiss
    • 1
  1. 1.Royal Aircraft EstablishmentFarnborough, Hants.UK

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