GPU CABARET Solutions for 30P30N Three-element High-lift Airfoil with Slat Modifications.
Author:
Affiliation:
1. Queen Mary University of London
2. University of Bristol
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2115
Reference53 articles.
1. Aeroacoustic Performance of High-lift Airfoil with Slat Cove Fillers
2. Experimental and numerical investigation of aerodynamic performance for airfoils with morphed trailing edges
3. Flow characteristics of slat cove fillers
4. Aerodynamic and aeroacoustic performance of high-lift airfoil fitted with slat cove fillers
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