Effect of trailing edge serration on the lift and drag characteristics of NACA0012 airfoil wing
Author:
Affiliation:
1. Ghulam Ishaq Khan Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4470
Reference7 articles.
1. A Method for Reducing the Base Drag of Wings with Blunt Trailing Edge
2. Vortex Shedding and Aerodynamic Performance of Airfoil with Multiscale Trailing-Edge Modifications
3. Particle-image velocimetry and force measurements of leading-edge serrations on owl-based wing models
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