Low-Order Modeling of Airfoils with Massively Separated Flow and Leading-Edge Vortex Shedding
Author:
Affiliation:
1. North Carolina State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0813
Reference34 articles.
1. Dynamic Stall in Pitching Airfoils: Aerodynamic Damping and Compressibility Effects
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