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Measurement of Rotorcraft Blade Deformation using Projection Moire InterferometryProjection Moire Interferometry (PMI) has been used to obtain near instantaneous, quantitative blade deformation measurements of a generic rotorcraft model at several test conditions. These laser-based measurements provide quantitative, whole field, dynamic blade deformation profiles conditionally sampled as a function of rotor azimuth. The instantaneous nature of the measurements permits computation of the mean and unsteady blade deformation, blade bending, and twist. The PMI method is presented, and the image processing steps required to obtain quantitative deformation profiles from PMI interferograms are described. Experimental results are provided which show blade bending, twist, and unsteady motion. This initial proof-of-concept test has demonstrated the capability of PMI to acquire accurate, full field rotorcraft blade deformation data.
Document ID
20040100752
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Fleming, Gary A.
(NASA Langley Research Center Hampton, VA, United States)
Gorton, Susan Althoff
(Army Aviation Systems Command Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1998
Subject Category
Aircraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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