NASA NTRS · 20160001627
Fiber Optic Rosette Strain Gauge Development and Application on a Large-Scale Composite Structure
Abstract
A 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.
Keep this discovery
Explore connections, maps & timelines
Moore, Jason P., Przekop, Adam, Juarez, Peter D., Roth, Mark C.. 2015-12-01. Fiber Optic Rosette Strain Gauge Development and Application on a Large-Scale Composite Structure. https://ntrs.nasa.gov/citations/20160001627
Cite the original work for its findings. Save a collection to share your selection of sources.