A self–tuning intelligent controller for a smart actuation mechanism of a morphing wing based on shape memory alloys
The paper exposes some of the results obtained in a major research project related to the
design, development, and experimental testing of a morphing wing demonstrator, with the …
design, development, and experimental testing of a morphing wing demonstrator, with the …
Unleashing the Potential of Morphing Wings: A Novel Cost Effective Morphing Method for UAV Surfaces, Rear Spar Articulated Wing Camber
The implementation of morphing wing applications in aircraft design has sparked significant
interest as it enables the dimensional properties of the aircraft to be modified during flight. By …
interest as it enables the dimensional properties of the aircraft to be modified during flight. By …
[HTML][HTML] Aerodynamic Analysis of Variable Camber-Morphing Airfoils with Substantial Camber Deflections
M Marciniuk, P Piskur, Ł Kiszkowiak, Ł Malicki… - Energies, 2024 - mdpi.com
In recent years, morphing wings have become not only a concept, but an aerodynamic
solution for the aviation industry to take a step forward toward future technologies. However …
solution for the aviation industry to take a step forward toward future technologies. However …
Numerical simulation of different aircraft sub-floor structures during ditching
B Wang, L Nie, Y Ren - The Aeronautical Journal, 2024 - cambridge.org
To enhance the impact resistance capacity and ensure the floatability of aircraft after
ditching, the slamming response of three types of aircraft sub-floor structures are …
ditching, the slamming response of three types of aircraft sub-floor structures are …
[PDF][PDF] Aerodynamic Impacts of Convergent Slot Implementation on Hinged and Morphed NACA 0012 Airfoil Operating at a High Reynolds Number
R Kumar, S Ghosh - Aeronautical System, 2025 - researchgate.net
Trailing-edge modifications on the NACA 0012 airfoil for lift enhancement are numerically
investigated at a Reynolds number 4.58× 106. Specifically, three variations in the trailing …
investigated at a Reynolds number 4.58× 106. Specifically, three variations in the trailing …