Electrospun electroactive polymers for aerospace applications

Kristin J. Pawlowski, Tyler L. St. Clair, Amber C. McReynolds, Cheol Park, Zoubeida Ounaies, Emilie J. Siochi, Joycelyn S. Harrison

Research output: Contribution to journalConference article

1 Scopus citations

Abstract

Electrospun 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.

Original languageEnglish (US)
Pages (from-to)3346-3350
Number of pages5
JournalCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Volume5
StatePublished - Aug 28 2003
Event44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference - Norfolk, VA, United States
Duration: Apr 7 2003Apr 10 2003

All Science Journal Classification (ASJC) codes

  • Architecture
  • Materials Science(all)
  • Aerospace Engineering
  • Mechanics of Materials
  • Mechanical Engineering

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  • Cite this

    Pawlowski, K. J., St. Clair, T. L., McReynolds, A. C., Park, C., Ounaies, Z., Siochi, E. J., & Harrison, J. S. (2003). Electrospun electroactive polymers for aerospace applications. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 5, 3346-3350.