High Aspect Ratio Multi-Stage Ducted Electroaerodynamic Thrusters for Micro Air Vehicle Propulsion
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Utah, Salt Lake City, UT, USA
2. Department of Electrical and Computer Engineering, University of Utah, Salt Lake City, UT, USA
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/7083369/10409903/10403976.pdf?arnumber=10403976
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1. Science, technology and the future of small autonomous drones
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