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Optical measurement of unducted fan blade deflectionsA nonintrusive optical method for measuring unducted fan (or propeller) blade deflections is described and evaluated. The measurement does not depend on blade surface reflectivity. Deflection of a point at the leading edge and a point at the trailing edge in a plane nearly perpendicular to the pitch axis is obtained with a single light beam generated by a low-power, helium-neon laser. Quantitative analyses are performed from taped signals on a digital computer. Averaging techniques are employed to reduce random errors. Measured static deflections from a series of high-speed wind tunnel tests of a counterrotating unducted fan model are compared with available, predicted deflections, which are also used to evaluate systematic errors.
Document ID
19910028423
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kurkov, A. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1990
Publication Information
Publication: ASME, Transactions, Journal of Turbomachinery
Volume: 112
ISSN: 0889-504X
Subject Category
Instrumentation And Photography
Report/Patent Number
ASME PAPER 89-GT-298
Accession Number
91A13046
Distribution Limits
Public
Copyright
Other

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