Publications
Electrical characteristics of wire-to-wire dielectric barrier discharges
Plasma Sources Sci. Technol. 30 08LT01
https://doi.org/10.1088/1361-6595/ac0a45
Higher thrust-to-power with large electrode gap spacing electroaerodynamic devices for aircraft propulsion
Journal of Physics D: Applied Physics, Volume 53, Number 2
https://doi.org/10.1088/1361-6463/ab4a4c
A dielectric barrier discharge ion source increases thrust and efficiency of electroaerodynamic propulsion
Appl. Phys. Lett. 114, 254105
https://doi.org/10.1063/1.5100524
Technical and environmental assessment of all-electric 180-passenger commercial aircraft
Progress in Aerospace Sciences Volume 105, February 2019, Pages 1-30
https://doi.org/10.1016/j.paerosci.2018.11.002
Energy, economic, and environmental prospects of all-electric aircraft
Nature Energy 4, 160–166
https://doi.org/10.1038/s41560-018-0294-x
Flight of an aeroplane with solid-state propulsion
Nature 563, 532–535
https://doi.org/10.1038/s41586-018-0707-9
Electroaerodynamic thruster performance as a function of altitude and flight speed
AIAA Journal
http://doi.org/10.2514/1.J056138
Electro-aerodynamic thrust for fixed-wing aircraft propulsion
PhD Thesis, Massachusetts Institute of Technology, DSpace @ MIT, September 2016
http://.doi.org/10.2514/1.J056138
Electrohydrodynamic thrust density using positive corona-induced ionic winds for in-atmosphere propulsion
Proceedings of the Royal Society A 471, 2015
doi: 10.1098/rspa.2014.0912
Economic and environmental assessment of liquefied natural gas as a supplemental aircraft fuel
Progress in Aerospace Sciences 66, pp 17-36, 2014
doi: 10.1016/j.paerosci.2013.12.002
On the performance of electrohydrodynamic propulsion
Proceedings of the Royal Society A 469 (2154), 2013
doi: 10.1098/rspa.2012.0623
Performance characterization of electrohydrodynamic propulsion devices
SM Thesis, Massachusetts Institute of Technology, DSpace @ MIT, September 2012
http://hdl.handle.net/1721.1/77114
Airframe design for ‘silent,’ fuel efficient aircraft
Journal of Aircraft 47 (3), pp 956-969, 2010
doi: 10.2514/1.46545