A dielectric barrier discharge ion source increases thrust and efficiency of electroaerodynamic propulsion-Reference-Cited by-同舟云学术

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A dielectric barrier discharge ion source increases thrust and efficiency of electroaerodynamic propulsion

Published:2019-06-24 Issue:25 Volume:114 Page:254105
ISSN:0003-6951
Container-title:Applied Physics Letters
language:en
Short-container-title:Appl. Phys. Lett.

Author:

Xu Haofeng¹,He Yiou²,Barrett Steven R. H.¹

Affiliation:

1. Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139, USA

2. Department of Electrical Engineering and Computer Science, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139, USA

Funder

Amar G. Bose Grant

Lincoln Laboratory, Massachusetts Institute of Technology

Publisher

AIP Publishing

Subject

Physics and Astronomy (miscellaneous)

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5100524

Reference26 articles.

1. Ion Drag Pumps

2. Ion Drag Pumping. I. Theory

3. Electrostatic Cooling of a Horizontal Cylinder

4. Design and optimization of electrostatic fluid accelerators

5. Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a One Atmosphere Uniform Glow Discharge Plasma

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