C Özel, E Özbek, S Ekici - International Journal of Aviation Science …, 2020 - dergipark.org.tr
Unmanned aerial vehicles (UAVs) have excelled with their ability to perform the intended task on or without personnel. In recent years, UAVs have been designed for civilian …
This work presents an aerodynamic optimization method for a Droop Nose Leading Edge (DNLE) and Morphing Trailing Edge (MTE) of a UAS-S45 root airfoil by using Bezier …
S Ameduri, A Concilio - Journal of Intelligent Material …, 2019 - journals.sagepub.com
Active blade twist is an option to increase helicopter performance, for instance moving its condition from hovering to cruise. Shape memory alloys give the possibility of realizing …
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 …
Flight range, endurance, maneuverability, and agility are the key elements that determine an aircraft's performance. Both conventional and morphing wing aircraft have been well studied …
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 …
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 …
View Video Presentation: https://doi. org/10.2514/6.2022-1038. vid In this paper, an overview is presented in the areas of Morphing Aircraft and Unmanned Aerial Systems …
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) …