Effect of Trailing-Edge Morphing on Flow Characteristics Around a Pitching Airfoil
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061055
Reference30 articles.
1. Flow physics and dynamics of flow-induced pitch oscillations of an airfoil
2. Dynamic Stall Experiments on Oscillating Airfoils
3. Investigation of flow over an oscillating airfoil
4. Dynamic stall simulation of a pitching airfoil under unsteady freestream velocity
5. Numerical investigations into the asymmetric effects on the aerodynamic response of a pitching airfoil
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