2017•Chinese Journal of AeronauticsRequires access

Optimization and design of a morphing wing tip aircraft demonstrator for drag reduction at low speeds, Part II – Experimental validation using infra-red transition measurements during wind tunnel tests

Andreea Koreanschi, Oliviu Şugar Gabor, Joran Acotto, Guillaume Brianchon, Gregoire Portier, Ruxandra Mihaela Botez, Mahmoud Mamou, Youssef Mébarki

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Key concepts: Morphing, Wind tunnel, Wing, Drag, Aerospace engineering, Reduction (mathematics), Engineering, Aerodynamics

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Optimization and design of a morphing wing tip aircraft demonstrator for drag reduction at low speeds, Part II – Experimental validation using infra-red transition measurements during wind tunnel tests — Research Paper | ScholarLens