Lift modeling and regulation for a finite wing during transverse gust encounters
Author:
Affiliation:
1. University of Maryland, College Park
2. State University of New York
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1146
Reference24 articles.
1. A Survey of Small-Scale Unmanned Aerial Vehicles: Recent Advances and Future Development Trends
2. Unsteady aerodynamics and flow control for flapping wing flyers
3. Experimental Study of Gust Effects on Micro Air Vehicles
4. Effect of Frontal Gusts on Forward Flapping Flight
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2. Quasi-Steady Effective Angle of Attack and Its Use in Lift-Equivalent Motion Design;AIAA Journal;2021-07
3. Effect of Three-Dimensional Geometry on Harmonic Gust–Airfoil Interaction;AIAA Journal;2021-02
4. Overview of NATO AVT-282: Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters;AIAA Scitech 2020 Forum;2020-01-05
5. The Unsteady Aerodynamics of a Transverse Wing-Gust Encounter with Closed-Loop Pitch Control;AIAA Scitech 2020 Forum;2020-01-05
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