Experimental investigation on a Trailing Edge Morphing Airfoil (TEMA) with zigzag rib structure at low speed
Camber-morphing wing technology enables adaptive adjustments to wing curvature by optimizing aerodynamic performance and efficiency for varying flight conditions. This study emphasizes the novel Trailing Edge Morphing Airfoil (TEMA) design and analysis, showcasing its noteworthy aerodynamic characte...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Universiti Putra Malaysia Press
2025
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| Online Access: | http://psasir.upm.edu.my/id/eprint/120960/ http://psasir.upm.edu.my/id/eprint/120960/1/120960.pdf |