Aerodynamic Analysis of Variable Camber-Morphing Airfoils with Substantial Camber Deflections
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, continuously morphing airfoils became an interesting answer to provide green
Marta Marciniuk +7 more
doaj +2 more sources
Experimental Validation and Evaluation of a Coupled Twist-Camber Morphing Wing Concept
A morphing wing concept allowing for coupled twist-camber shape adaptation is proposed. The design is based on an optimized thickness distribution both spanwise and chordwise to be able to morph the wing sections into targeted airfoil shapes ...
Afzal Suleman, José Lobo do Vale
exaly +3 more sources
The Conceptual Design of a Variable Camber Wing [PDF]
The variable camber wing (VCW) is a morphing wing design anticipated to enhance unmanned aerial vehicles’ (UAVs’) performance in flight through continuously changing shape.
Spencer Troy P. Cortez +2 more
doaj +2 more sources
Numerical Investigation of an NACA 13112 Morphing Airfoil [PDF]
This article presents a numerical study on the 2D aerodynamic characteristics of an airfoil with a morphed camber. The operational regime of the main rotor blade of the IAR 330 PUMA helicopter was encompassed in CFD simulations, performed over an angle ...
Mădălin-Dorin Feraru +3 more
doaj +2 more sources
Kinematic Simulation and Structure Analysis of a Morphing Flap [PDF]
This thesis presents a study on the design and analysis of a morphing flap structure integrated with actuation mechanism for potential application to large aircraft.
Guo, Shixian
core +7 more sources
Design and Validation of the Trailing Edge of a Variable Camber Wing Based on a Two-Dimensional Airfoil [PDF]
Variable camber wing technology stands out as the most promising morphing technology currently available in green aviation. Despite the ongoing advancements in smart materials and compliant structures, they still fall short in terms of driving force ...
Jin Zhou +6 more
doaj +2 more sources
Computational Analysis of 3D Lattice Structures for Skin in Real-Scale Camber Morphing Aircraft
Conventional or fixed wings require a certain thickness of skin material selection that guarantees structurally reliable strength under expected aerodynamic loadings.
Muhammad Akbar
exaly +3 more sources
Analysis of composite wing structures with a morphing leading edge [PDF]
One of the main challenges for the civil aviation industry is the reduction of its environmental impact. Over the past years, improvements in performance efficiency have been achieved by simplifying the design of the structural components and using ...
Morishima, Ryoko
core +7 more sources
Optimal design of a composite active aeroelastic wing [PDF]
The primary aim of this research was to design a Seamless Aeroelastic Wing (SAW) structure applicable to a lightweight Unmanned Aerial Vehicle (UAV). Therefore the study focused on optimal design of a SAW structure by utilising the maximum aeroelastic ...
Perera, Melanie
core +7 more sources
Development of aeroelastic modeling and analysis for wing camber morphing technology
As one of the morphing methods, wing camber morphing technology has received great attention. Starting from the relevant projects of morphing wing at home and abroad, the aeroelastic modeling and analysis means of the camber morphing technology are ...
NI Yingge +3 more
doaj +1 more source

