Time-Delayed Active Control of Stall Flutter for an Airfoil via Camber Morphing-Reference-Cited by-同舟云学术

Time-Delayed Active Control of Stall Flutter for an Airfoil via Camber Morphing

Published:2022-10 Issue:10 Volume:60 Page:5723-5734
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Wu You¹,Dai Yuting¹,Yang Chao¹

Affiliation:

1. Beihang University, 100191 Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Academic Excellence Foundation of BUAA for PhD Students

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J061947

Reference26 articles.

1. HalfmanR. L.JohnsonH. C.HaleyS. M. “Evaluation of High-Angle-of-Attack Aerodynamic Derivative Data and Stall-Flutter Prediction Techniques,” NACA TN 2533, 1951.

2. Bifurcation Behavior of Airfoil Undergoing Stall Flutter Oscillations in Low-Speed Wind Tunnel

3. AERODYNAMICS OF SMALL VEHICLES

4. Self-sustained aeroelastic oscillations of a NACA0012 airfoil at low-to-moderate Reynolds numbers

5. Stall flutter of NACA 0012 airfoil at low Reynolds numbers

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