Status and challenges on design and implementation of camber morphing mechanisms
T Majid, BW Jo - International Journal of Aerospace …, 2021 - Wiley Online Library
This paper presents state‐of‐the‐art technologies of camber morphing mechanisms from the
perspectives of design and implementation. Wing morphing technologies are aimed at …
perspectives of design and implementation. Wing morphing technologies are aimed at …
Review of adaptive shock control systems
SC Künnecke, S Vasista, J Riemenschneider… - Applied Sciences, 2021 - mdpi.com
Drag reduction plays a major role in future aircraft design in order to lower emissions in
aviation. In transonic flight, the transonic shock induces wave drag and thus increases the …
aviation. In transonic flight, the transonic shock induces wave drag and thus increases the …
Integrated design of a morphing winglet for active load control and alleviation of turboprop regional aircraft
Aircraft winglets are well-established devices that improve aircraft fuel efficiency by enabling
a higher lift over drag ratios and lower induced drag. Retrofitting winglets to existing aircraft …
a higher lift over drag ratios and lower induced drag. Retrofitting winglets to existing aircraft …
Augmented aircraft performance with the use of morphing technology for a turboprop regional aircraft wing
F Moens - Biomimetics, 2019 - mdpi.com
This article presents some application of the morphing technology for aerodynamic
performance improvement of turboprop regional aircraft. It summarizes the results obtained …
performance improvement of turboprop regional aircraft. It summarizes the results obtained …
Optimization and design of a flexible droop-nose leading-edge morphing wing based on a novel black widow optimization algorithm—Part I
An aerodynamic optimization for a Droop-Nose Leading-Edge (DNLE) morphing of a well-
known UAV, the UAS-S45, is proposed, using a novel Black Widow Optimization (BWO) …
known UAV, the UAS-S45, is proposed, using a novel Black Widow Optimization (BWO) …
Optimization of compliant adaptive structures in the design of a morphing droop nose
V Cavalieri, A De Gaspari, S Ricci - Smart Materials and …, 2020 - iopscience.iop.org
A design procedure for the synthesis of active camber morphing wing devices is proposed. A
topology optimization initially defines the internal structure that is further enhanced by …
topology optimization initially defines the internal structure that is further enhanced by …
Performance improvements of a regional aircraft by riblets and natural laminar flow
The application of riblets on a typical regional turboprop configuration is discussed in this
paper. The effect of the riblets is modeled as a singular roughness problem by a proper …
paper. The effect of the riblets is modeled as a singular roughness problem by a proper …
Gradient-based aerodynamic optimization of an airfoil with morphing leading and trailing edges
Z Zhang, A De Gaspari, S Ricci, C Song, C Yang - Applied Sciences, 2021 - mdpi.com
This article presents a gradient-based aerodynamic optimization framework and investigates
optimum deformations for a transonic airfoil equipped with morphing leading and trailing …
optimum deformations for a transonic airfoil equipped with morphing leading and trailing …
Investigation of the effective factors on solar powered fixed-wing UAV for extended flight endurance
A Alfalari, Y Alaiwi - 2022 International Symposium on …, 2022 - ieeexplore.ieee.org
In recent years, big interest of wing geometry emerged because it affects all other aircraft
components. Geometry affects aircraft forces due to airflow characteristics. Solar cells …
components. Geometry affects aircraft forces due to airflow characteristics. Solar cells …
Advanced Design of a Full‐Scale Active Morphing Droop Nose
A De Gaspari, V Cavalieri… - International Journal of …, 2020 - Wiley Online Library
This paper describes the design of a morphing droop nose conceived to increase the
performance in high‐lift conditions of a twin‐prop regional aircraft, while ensuring the natural …
performance in high‐lift conditions of a twin‐prop regional aircraft, while ensuring the natural …