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Fiber Optic Rosette Strain Gauge Development and Application on a Large-Scale Composite StructureA detailed description of the construction, application, and measurement of 196 FO rosette strain gauges that measured multi-axis strain across the outside upper surface of the forward bulkhead component of a multibay composite fuselage test article is presented. A background of the FO strain gauge and the FO measurement system as utilized in this application is given and results for the higher load cases of the testing sequence are shown.
Document ID
20160001627
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Moore, Jason P.
(NASA Langley Research Center Hampton, VA, United States)
Przekop, Adam
(NASA Langley Research Center Hampton, VA, United States)
Juarez, Peter D.
(NASA Langley Research Center Hampton, VA, United States)
Roth, Mark C.
(Modern Machine and Tool Co. Newport News, VA, United States)
Date Acquired
February 5, 2016
Publication Date
December 1, 2015
Subject Category
Aircraft Design, Testing And Performance
Instrumentation And Photography
Report/Patent Number
NF1676L-22973
L-20627
NASA/TM-2015-218970
Report Number: NF1676L-22973
Report Number: L-20627
Report Number: NASA/TM-2015-218970
Funding Number(s)
WBS: WBS 338881.02.22.07.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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