Numerical Investigation of the Trailing Edge Morphing Using Corrugated Skin at a High Reynolds Number for NACA 0012 & NACA 641-612 Airfoils
AIAA Aviation Forum ; 2023 ; San Diego, Calif.; Online
2023
Aufsatz (Konferenz)
Englisch
Chordwise Actuation Effects on NACA 0012 Morphing Airfoils (AIAA 2018-3957)
British Library Conference Proceedings | 2018
|