Mechanisms for Turbulent-Separation-Control at Reynolds Number of 1.6×106 using Vortex-Generator-Type Plasma Actuators - Comparison with Spanwise-Type Plasma Actuators
AIAA AVIATION 2022 Forum
01.01.2022
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Experimental Comparison of DBD Plasma Actuators for Low Reynolds Number Separation Control
Online Contents | 2013
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