T Majid, BW Jo - Applied Sciences, 2021 - mdpi.com
This paper aims to numerically validate the aerodynamic performance and benefits of variable camber rate morphing wings, by comparing them to conventional ones with plain …
Piezoelectric Ultrasonic motors (USM) are based on the principle of converse piezoelectric effect ie, vibrations occur when an electrical field is applied to piezoelectric materials. USMs …
A Zhao, H Zou, H Jin, D Wen - Aerospace Science and Technology, 2019 - Elsevier
A whole adaptive variable camber wing (AVCW) equipped with an innovative double rib sheet (DRS) structure is experimentally and numerically studied in this work. The DRS …
S Das, P Kunjam, B Moling, T Gao… - Interface …, 2024 - royalsocietypublishing.org
Morphing materials are typically either very compliant to achieve large shape changes or very stiff but with small shape changes that require large actuation forces. Interestingly, fish …
The seamless trailing edge morphing flap is investigated using a high-fidelity steady-state aerodynamic shape optimization to determine its optimum configuration for different flight …
Avian wings are characterized by intricate feather movements to manipulate airflow and enhance aerodynamic performance. The wing trailing-edge undergoes continuous gradual …
G Cheng, T Ma, J Yang, N Chang, X Zhou - Aerospace, 2023 - mdpi.com
Morphing trailing edge wing as an important morphing wing technology has gained wide attention because of its advantages, such as gust mitigation, improved aerodynamic …
In this paper, the authors analyze an important but overlooked area, the aerodynamics of the variable camber morphing wing in transition, where 6% camber changes from 2% to 8 …
R Wang, X Ma, G Zhang, P Ying… - Journal of Aerospace …, 2023 - ascelibrary.org
The present study numerically investigates the aerodynamic performance of the morphing airfoil and wing with leading edge (LE) and trailing edge (TE) parabolic flaps. Reynolds …