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What is Ionic Wind Propulsion in Aircraft about?

This paper presents a numerical investigation of an electroaerodynamic driven aeroplane using a unipolar ion drift model coupled with Navier–Stokes equations. The study analyzes the electrical properties, ionic wind generation, and flight performance of the aeroplane, highlighting the importance of matching electrical and flight parameters for optimal performance. The results indicate that ionic wind propulsion offers a promising alternative to traditional fossil-fuel-based propulsion systems.

Author

czapeczka

Language

EN