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
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