Further Investigations of Vortical Gust/Airfoil Interactions at a Transitional Reynolds Number
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0823
Reference27 articles.
1. High-Fidelity Simulations of Transitional Airfoil Interacting with Upstream Vortical Structure
2. Exploration of plasma-based control for low-Reynolds number airfoil/gust interaction
3. Implicit LES Computation of a Vortical-Gust/Wing Interaction for Transitional Flow
4. Impact of a Vortical Gust on the Aerodynamics of a Finite Aspect-Ratio Wing
5. Self-Sustained Pitch-Heave Oscillations and Gust Response of an Airfoil at Transitional Reynolds Numbers
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1. Overview of NATO AVT-282: Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters;AIAA Scitech 2020 Forum;2020-01-05
2. Further Investigation on the Effect of Sweep on Parallel Vortical-Gust/Wing Interactions on a Finite Aspect-Ratio Wing;AIAA Aviation 2019 Forum;2019-06-15
3. Vortical Gusts: Experimental Generation and Interaction with Wing;AIAA Journal;2019-03
4. Computational Investigation of the Effect of Sweep on Parallel Vortical-Gust/Wing Interactions;AIAA Scitech 2019 Forum;2019-01-06
5. Clockwise Vortical-Gust/Airfoil Interactions at a Transitional Reynolds Number;AIAA Journal;2018-10
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