A novel method to predict current–voltage characteristics of positive corona discharges based on a perturbation technique. II. Global analysis and applications to electrohydrodynamic thrusters
Source abstract
Abstract
Electrohydrodynamic (EHD) thrusters can silently propel small unmanned aerial vehicles without moving parts using corona discharges. Computational fluid dynamics would be a powerful tool to model the EHD thrusters and then optimize them. The drift-diffusion-Poisson equations govern corona discharges; hence, the equations can predict the current–voltage characteristics curves of EHD thrusters. However, the equations are too stiff to analyze EHD thrusters in the time domain. Here, we propose a perturbation technique to efficiently solve the stiff drift-diffusion-Poisson system in global (i.e., full two-dimensional or three-dimensional) and nonlinear (i.e., applied voltages higher than the corona inception voltage) regimes. Furthermore, we validated the method with the experimental results of a previous study.
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Research context
OpenAlex topics: Aerosol Filtration and Electrostatic Precipitation · High voltage insulation and dielectric phenomena · Electrohydrodynamics and Fluid Dynamics
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Department of Radiology, The University of Tokyo Hospital 1 , 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8655, Japan
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (ISAS/JAXA) 2 , 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, Kanagawa 252-5210, Japan
References (20)
Show source-provided references
1. Flight of an aeroplane with solid-state propulsion10.1038/s41586-018-0707-9 ↗
2. On the performance of electrohydrodynamic propulsion10.1098/rspa.2012.0623 ↗
3. Electrohydrodynamic thrust density using positive corona-induced ionic winds for in-atmosphere propulsion10.1098/rspa.2014.0912 ↗
4. Higher thrust-to-power with large electrode gap spacing electroaerodynamic devices for aircraft propulsion10.1088/1361-6463/ab4a4c ↗
5. Ion-neutral propulsion in atmospheric media10.2514/3.4302 ↗
6. On the influence that the ground electrode diameter has in the propulsion efficiency of an asymmetric capacitor in nitrogen gas10.1063/1.3562874 ↗
7. Simulation of a wire-cylinder-plate positive corona discharge in nitrogen gas at atmospheric pressure10.1063/1.4725499 ↗
8. Modeling of an EHD corona flow in nitrogen gas using an asymmetric capacitor for propulsion10.1016/j.elstat.2011.02.002 ↗
9. Modeling of an improved positive corona thruster and actuator10.1016/j.elstat.2012.09.001 ↗
10. Performance prediction of electrohydrodynamic thrusters by the perturbation method10.1063/1.4951721 ↗
11. A novel method to predict current voltage characteristics of positive corona discharges based on a perturbation technique. I. Local analysis10.1063/1.4995025 ↗
12. Electrostatic propulsion device for aerodynamics applications10.1063/1.4958815 ↗
13. Single-stage EHD thruster response to several simulation conditions in nitrogen gas10.1063/1.4986219 ↗
14. Study of the design and efficiency of single stage EHD thrusters at the sub-atmospheric pressure of 1.3 kPa10.1063/1.5018424 ↗
15. Global stability analysis method to numerically predict precursor of breakdown voltage10.1088/0963-0252/24/5/055014 ↗
16. Streamline upwind/Petrov–Galerkin formulations for convection dominated flows with particular emphasis on the incompressible Navier-Stokes equations10.1016/0045-7825(82)90071-8 ↗
17. A practical guide to modeling low-current quasi-stationary gas discharges: Eigenvalue, stationary, and time-dependent solvers10.1063/5.0057856 ↗
18. 1998
19. Solving unsymmetric sparse systems of linear equations with PARDISO10.1016/j.future.2003.07.011 ↗
20. Direct current breakdown in gases for complex geometries from high vacuum to atmospheric pressure10.1088/0022-3727/46/28/285205 ↗