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...

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Bibliographic Details

Main Authors:	Kodigaddi, Siddalingappa Parameshappa, Venkataramana, Srikanth Holalu, Natesan, Kapilan, Mazlan, Norkhairunnisa
Format:	Article
Language:	en
Published:	Universiti Putra Malaysia Press 2025
Online Access:	http://psasir.upm.edu.my/id/eprint/120960/1/120960.pdf http://psasir.upm.edu.my/id/eprint/120960/ http://pertanika2.upm.edu.my/pjst/browse/regular-issue?article=JST-5100-2024
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