VIRTUAL WALL OSCILLATIONS FORCED BY A DBD PLASMA ACTUATOR OPERATING UNDER BEAT FREQUENCY - A CONCEPT FOR TURBULENT DRAG REDUCTION

VIRTUAL WALL OSCILLATIONS FORCED BY A DBD PLASMA ACTUATOR OPERATING UNDER BEAT FREQUENCY - A CONCEPT FOR TURBULENT DRAG REDUCTION

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Veröffentlicht in:AIAA Aviation Forum (2020 : Online) Flow control
1. Verfasser: Hehner, Marc T. (VerfasserIn)
Weitere Verfasser: Gatti, Davide (VerfasserIn), Mattern, Philipp (VerfasserIn), Kotsonis, Marios (VerfasserIn), Kriegseis, Jochen (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2020
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