Experimental Study of Aerodynamic Characteristics of Partially Flexible NACA0012 Airfoil
Author:
Affiliation:
1. University of Shanghai for Science and Technology, 200093 Shanghai, 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.J061803
Reference20 articles.
1. Experimental investigation of the flow past passive vortex generators on an airfoil experiencing three-dimensional separation
2. Flow control on the NREL S809 wind turbine airfoil using vortex generators
3. Aerodynamic optimization and mechanism design of flexible variable camber trailing-edge flap
4. Numerical Study of Wings With Wavy Leading and Trailing Edges
5. Numerical optimization and experimental validation for a tidal turbine blade with leading-edge tubercles
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