Results 11 to 20 of about 862 (246)

Optimal design of watt six-bar transmission mechanism for morphing trailing edge [PDF]

open access: yesE3S Web of Conferences, 2021
The morphing trailing edge could realize a continuous smooth deformation compared with conventional trailing edge, which effectively improves the aerodynamic performance.
Zhou Jin, Zhao Shiwei
doaj   +2 more sources

Aerodynamic Shape Optimization of an Adaptive Morphing Trailing Edge Wing [PDF]

open access: yes15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2014
Adaptive morphing trailing-edge wings have the potential to reduce the fuel burn of transport aircraft. However, to take full advantage of this technology and to quantify its benefits, design studies are required. To address this need, the aerodynamic performance benefits of a morphing trailing-edge wing are quantified using aerodynamic design ...
Lyu, Zhoujie, Martins, Joaquim R. R. A.
openaire   +3 more sources

Aerodynamic Performance of Morphing and Periodic Trailing-Edge Morphing Airfoils in Ground Effect [PDF]

open access: yesJournal of Aerospace Engineering, 2023
Applying fish bone active camber morphing to the wing-in-ground effect to improve the aerodynamic efficiency was investigated using computational fluid dynamics (CFD) at a Reynolds number of 320,000. Steady-static morphing was first carried out with Reynolds-averaged Navier–Stokes (RANS) equations in two dimensions for morphing start locations off (60%,
Dominic Clements, Kamal Djidjeli
openaire   +3 more sources

Morphing wing design using integrated and distributed trailing edge morphing

open access: yesSmart Materials and Structures, 2022
Abstract The presented study investigates the design and development of an autonomous morphing wing concept developed in the scope of the SmartX project, which aims to demonstrate in-flight performance optimisation with active morphing.
Tigran Mkhoyan   +3 more
openaire   +4 more sources

3D-Printed Wings with Morphing Trailing-Edge Technology

open access: yesAIAA Scitech 2021 Forum, 2021
In recent years, various groups have attempted to improve aircraft efficiency using wings with morphing trailing-edge technology. Most of these solutions are difficult to manufacture or have limited morphing capability. The present paper outlines a research effort to develop an easy to manufacture, fully 3D-printed morphing wing.
Moulton, Benjamin C.   +1 more
openaire   +5 more sources

Static Aeroelastic Characteristics of Morphing Trailing-Edge Wing Using Geometrically Exact Vortex Lattice Method

open access: yesInternational Journal of Aerospace Engineering, 2019
A morphing trailing-edge (TE) wing is an important morphing mode in aircraft design. In order to explore the static aeroelastic characteristics of a morphing TE wing, an efficient and feasible method for static aeroelastic analysis has been developed in ...
Sen Mao   +3 more
doaj   +2 more sources

Aerostructural Design Optimization of an Adaptive Morphing Trailing Edge Wing [PDF]

open access: yes56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2015
Adaptive morphing trailing edge technology offers the potential to decrease the fuel burn of transonic transport aircraft by allowing wings to dynamically adjust to changing flight conditions. Current aircraft use flap and aileron droop to adjust the wing during flight.
David A. Burdette   +3 more
openaire   +2 more sources

Design of a Smart Morphing Wing Using Integrated and Distributed Trailing Edge Camber Morphing

open access: yesASME 2020 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, 2020
Abstract In this study, the design and development of an autonomous morphing wing concept were investigated. This morphing wing was developed in the scope of, the Smart-X project, aiming to demonstrate in-flight performance optimisation.
Mkhoyan, T. (author)   +3 more
openaire   +4 more sources

Experimental investigation of aerodynamic performance of airfoils fitted with morphing trailing edges [PDF]

open access: yes54th AIAA Aerospace Sciences Meeting, 2016
The aerodynamic performance and wake development of a NACA 0012 airfoil fitted with morphing trailing edges were studied using experimental and computational techniques. The NACA 0012 airfoil was tested with morphing trailing edges having various camber profiles with the same trailing edge tip deflection.
Ai, Qing   +2 more
openaire   +4 more sources

Decamber Morphing Concepts by Using a Hybrid Trailing Edge Control Surface [PDF]

open access: yesAerospace, 2015
The idea of morphing is drawing extensive attention in aerospace technologies. Several different approaches like span, camber, twist, and sweep are finding applications.
Yavuz Yaman   +8 more
doaj   +3 more sources

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