Unsteady CFD simulations for Active Flow Control
Author:
Affiliation:
1. University of Strasbourg
2. CFS Engineering
3. Insitute de Mecanique des Fluides de Toulouse
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2854
Reference33 articles.
1. Numerical investigation of frequency-amplitude effects of dynamic morphing for a high-lift configuration at high Reynolds number
2. Morphing of a supercritical wing by means of trailing edge deformation and vibration at high Reynolds numbers: Experimental and numerical investigation
3. Shock-vortex shear-layer interaction in the transonic flow around a supercritical airfoil at high Reynolds number in buffet conditions
4. Dynamics of a hybrid morphing wing with active open loop vibrating trailing edge by time-resolved PIV and force measures
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