Numerical Investigation of the Trailing Edge Morphing using Corrugated Skin at a High Reynolds Number for NACA 0012 & NACA 64(1)-612 Airfoils
AIAA AVIATION 2023 Forum
2023-01-01
Conference paper
Electronic Resource
English
Chordwise Actuation Effects on NACA 0012 Morphing Airfoils (AIAA 2018-3957)
British Library Conference Proceedings | 2018
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