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Electrospun Electroactive Polymers for Aerospace ApplicationsElectrospun piezoelectric polymers are being developed for use as a component on lightweight wings for micro-air vehicles (MAV). The goal is to incorporate fibers with tailored properties to permit dynamic control and maneuverability during flight. In particular, electrospun fiber mats of two piezoelectric polymers were investigated to ascertain their potential for the MAV application. In the work reported here, the typical experimental set-up for electrospinning was modified to induce fiber orientation in the spun mats. The morphologies of the resulting fibers and fiber mats were evaluated for various experimental conditions, and a comparison between oriented and unoriented fiber mats was carried out.
Document ID
20040085790
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Pawlowski, Kristin J.
(NASA Langley Research Center Hampton, VA, United States)
St.Clair, Tyler L.
(Mary Washington Coll. Fredricksburg, VA, United States)
McReynolds, Amber C.
(NASA Langley Research Center Hampton, VA, United States)
Park, Cheol
(National Inst. of Aerospace Hampton, VA, United States)
Ounaies, Zoubeida
(Virginia Commonwealth Univ. Richmond, VA, United States)
Siochi, Emilie J.
(NASA Langley Research Center Hampton, VA, United States)
Harrison, Joycelyn S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Nonmetallic Materials
Report/Patent Number
AIAA Paper 2003-1768
Report Number: AIAA Paper 2003-1768
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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