Full metadata
Title
Ionic Wind Propulsion
Description
This paper describes the research done to attempt to scale up thrusts produced by ionic wind thrusters, or "lifters" to magnitudes needed to power a 2 kg hobbyist remote-control airplane. It includes background information on the Biefeld-Brown effect and the thrust it produces, an experiment that attempted to prove that thrust can be scaled up from smaller ionic wind thrusters to larger scales, and two models predicting thruster geometries and power sources needed to reach these thrusts. An ionic wind thruster could not be created that would power the hobbyist remote as a high-voltage power source with voltage and power high enough could not be obtained. Thrusters were created for the experiment using balsa wood, aluminum foil, and thin copper wire, and were powered using a 30 kV transformer. The thrusters attempted to test for correlations between thrust, electrode length, and current; electric field strength, and thrust; and thrust optimization through opening up air flow through the collector electrode. The experiment was inconclusive as all the thrusters failed to produce measurable thrust. Further experimentation suggests the chief failure mode is likely conduction from the collector electrode to the nearby large conductive surface of the scale.
Date Created
2017-12
Contributors
- Haug, Andrew James (Author)
- White, Daniel (Thesis director)
- Takahashi, Timothy (Committee member)
- Middleton, James (Committee member)
- Mechanical and Aerospace Engineering Program (Contributor)
- Department of Military Science (Contributor)
- Barrett, The Honors College (Contributor)
Topical Subject
Resource Type
Extent
18 pages
Language
eng
Copyright Statement
In Copyright
Primary Member of
Series
Academic Year 2017-2018
Handle
https://hdl.handle.net/2286/R.I.45974
Level of coding
minimal
Cataloging Standards
System Created
- 2017-12-05 11:00:03
System Modified
- 2021-08-11 04:09:57
- 3 years 3 months ago
Additional Formats