• DocumentCode
    2902939
  • Title

    An optical deflectometer for the quantitative analysis of turbulent structures

  • Author

    McIntyre, S.S. ; Stanewsky, E. ; Settles, G.S.

  • Author_Institution
    Gas Dynamics Lab., Pennsylvania State Univ., University Park, PA, USA
  • fYear
    1991
  • fDate
    27-31 Oct 1991
  • Firstpage
    34
  • Lastpage
    42
  • Abstract
    The optical deflectometer is proposed to make turbulence measurements. The instrument, which is based on the schlieren principle, is nonintrusive and has a practically unlimited frequency response. Its novelty also lies in the fact that it produces a real image of the flowfield under study, in which optical probes may be positioned precisely. This instrument has been successfully applied in studying the turbulent mixing layers of both a low-speed CO2 jet and highly compressible Mach 3 airjet. The results are shown to be consistent over a broad range of knife-edge cutoff settings, and are comparable to turbulence data obtained by other more standard turbulence instruments. The major limitation of the optical deflectometer, in its present embodiment, is the fact that it integrates fluctuations across the flow
  • Keywords
    flow measurement; fluctuations; jets; nonelectric sensing devices; probes; schlieren systems; turbulence; CO2 jet; compressible Mach 3 airjet; flow measurement; fluctuations; frequency response; knife-edge cutoff settings; optical deflectometer; optical probes; quantitative analysis; schlieren instrument; turbulence measurements; turbulent mixing layers; turbulent structures; Frequency response; High speed optical techniques; Image motion analysis; Instruments; Laboratories; Large-scale systems; Mechanical engineering; Optical mixing; Optical sensors; Probes;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 1991. ICIASF '91 Record., International Congress on
  • Conference_Location
    Rockville, MD
  • Type

    conf

  • DOI
    10.1109/ICIASF.1991.186222
  • Filename
    186222