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Holographic testing of composite propfans for a cruise missile wind tunnel modelEach of the approximately 90 composite propfan blades constructed for a 55 percent scale cruise missile wind tunnel model were holographically tested to obtain natural frequencies and mode shapes. These data were used not only for quality assurance, but also to select sets of similar blades for each blade row. Presented along with the natural frequency data is a description of a computer-based image processing system developed to supplement the photographic based system for holographic image analysis and storage. The new system is quicker and cheaper, the holograms are indexed better, and several engineers can access the data simultaneously. The only negative effect is a slight reduction in image resolution, which does not influence the end use.
Document ID
19940019072
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Miller, Christopher J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-105271
NAS 1.15:105271
E-8203
Report Number: NASA-TM-105271
Report Number: NAS 1.15:105271
Report Number: E-8203
Accession Number
94N23545
Funding Number(s)
PROJECT: RTOP 535-03-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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