Thrust generation by a low-pressure plasma actuator
The property of plasma actuators to generate an airflow without moving parts gives them the potential to be used as a method of contamination control in low-pressure ultra-clean environments. This work describes and shows a measurement technique—based on deflection of microparticles—for determining the air flow induced by a plasma actuator at low pressures in air. Using this technique, the generated thrust is measured at varying pressures ranging from 1 to 25 mbar and for different electrical powers delivered to the plasma. Simultaneously, the measurement technique proves the capability of using this airflow to deflect particles for contamination control purposes; with a thrust up to 7.7±0.4×10−6mNm−1 at 1 mbar and a plasma power of 0.41±0.01 W, we demonstrate that plasma actuators generate enough thrust, even at low pressures, to deflect particles several millimeters on time scales less than a second.
Authors
- J. Beckers
- P. Blom
- G. B. Klaassen (ORCID: https://orcid.org/0000-0001-5212-955X)
- G. L. A. 't Lam (ORCID: https://orcid.org/0009-0003-7492-2569)
- B. Dol (ORCID: https://orcid.org/0009-0005-4509-1430)
Institutions
- Eindhoven University of Technology (NL)
Publication Details
- Journal
- Physics of Plasmas
- Published
- 2026-05-01
- DOI
- https://doi.org/10.1063/5.0311024
- Primary Topic
- Plasma and Flow Control in Aerodynamics
- Type
- article
- Field-Weighted Citation Impact
- 0.00
Funders
- Nederlandse Organisatie voor Wetenschappelijk Onderzoek