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Combined fringe and Fabry-Perot laser anemometer for 3 component velocity measurements in turbine stator cascade facilityA laser anemometer is described that was developed for use in a 508 mm diameter annular turbine stator cascade facility. All three velocity components are measured through a single restricted optical port, both within the stator vane row and downstream of the vanes. The measurements are made through a cylindrical window in the casing that matches the tip radius of the cascade. The stator tested has a contoured hub endwall that results in a large radial flow near the hub. The anemometer uses a standard fringe configuration (LFA) with a fluorescent aerosol seed to measure the axial and circumferential velocity components. The radial component is measured with a confocal Fabry-Perot interferometer. The two configurations are combined in a single optical system and can operate simultaneously. Data are presented to illustrate the capabilities of the system.
Document ID
19870011750
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Seasholtz, Richard G.
(NASA Lewis Research Center Cleveland, OH, United States)
Goldman, Louis J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1986
Publication Information
Publication: AGARD Advanced Instrumentation for Aero Engine Components
Subject Category
Engineering (General)
Accession Number
87N21183
Distribution Limits
Public
Copyright
Other
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