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Three component laser anemometer measurements in an annular cascade of core turbine vanes with contoured end wallThe three mean velocity components were measured in a full-scale annular turbine stator cascade with contoured hub end wall using a newly developed laser anemometer system. The anemometer consists of a standard fringe configuration using fluorescent seed particles to measure the axial and tangential components. The radial component is measured with a scanning confocal Fabry-Perot interferometer. These two configurations are combined in a single optical system that can operate simultaneously in a backscatter mode through a single optical access port. Experimental measurements were obtained both within and downstream of the stator vane row and compared with calculations from a three-dimensional inviscid computer program. In addition, detailed calibration procedures are described that were used, prior to the experiment, to accurately determine the laser beam probe volume location relative to the cascade hardware.
Document ID
19890001473
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Goldman, Louis J.
(NASA Lewis Research Center Cleveland, OH, United States)
Seasholtz, Richard G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
E-4183
NAS 1.60:2846
NASA-TP-2846
Report Number: E-4183
Report Number: NAS 1.60:2846
Report Number: NASA-TP-2846
Accession Number
89N10844
Funding Number(s)
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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