Results 91 to 100 of about 2,913 (212)

Design, Manufacturing and Test of a High Lift Secondary Flight Control Surface with Shape Memory Alloy Post-Buckled Precompressed Actuators

open access: yesActuators, 2015
The use of morphing components on aerospace structures can greatly increase the versatility of an aircraft. This paper presents the design, manufacturing and testing of a new kind of adaptive airfoil with actuation through Shape Memory Alloys (SMA ...
Thomas Sinn, Ron Barrett
doaj   +1 more source

Construction of a Morphing Wing Rib Actuated by a NiTi Wire

open access: yesJournal of Aerospace Technology and Management, 2015
The main goal of this paper is to analyze if it is feasible to employ a trained shape memory alloy wire as a linear actuator to modify the camber of a morphing wing rib.
Thais Campos de Almeida   +2 more
doaj  

Topology Design of Pressure Adaptive Honeycomb for a Morphing Fowler Flap

open access: yes52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2011
A new method for designing a morphing Fowler flap based on pressure-adaptive honeycomb is detailed. Pressure adaptive honeycomb has been shown to be able to induce gross camber deformations in airfoil sections, such as a flap. However, due to the large amount of design variables the integration of the honeycomb as a distributed actuator in a flap ...
Scheepstra, J. (author)   +2 more
openaire   +3 more sources

Mathematical modeling and control of a tilt-rotor aircraft

open access: yes, 2015
This paper presents a novel model of large-size tilt-rotor aircraft, which can operate as a helicopter as well as being capable of transition to fixed-wing flight.
Cai, Lilong, Wang, Xinhua
core   +2 more sources

Optimization and Experimental Investigation of a Single-Actuation Compliant Morphing Trailing Edge for Multiple Aerodynamic Configurations

open access: yesActuators
This work presents a low-fidelity optimization method for a compliant morphing wing trailing-edge structure, developed to achieve multiple optimized aerodynamic shapes under combined aerodynamic and control loads using a single actuation pathway ...
Martynas Lendraitis   +1 more
doaj   +1 more source

Design and Optimization of a Compliant Morphing Trailing Edge for High-Lift Generation

open access: yesApplied Sciences
This work focuses on the design and optimization of a morphing-compliant system developed within the project HERWINGT (Clean Aviation) and aimed at generating high lift during take-off and landing.
Salvatore Ameduri   +11 more
doaj   +1 more source

Advanced Aerodynamic Technologies for Future Green Regional Aircraft

open access: yesINCAS Bulletin, 2014
Future Green Regional Aircraft (GRA) will operate over airports located in the neighborhood of densely populated areas, with high frequency of takeoff/ landing events and, hence, strongly contribute to community noise and gaseous emissions.
Catalin NAE
doaj   +1 more source

Validation of the Lockheed Martin Morphing Concept with Wind Tunnel Testing [PDF]

open access: yes
The Morphing Aircraft Structures (MAS) program is a Defense Advanced Research Projects Agency (DARPA) led effort to develop morphing flight vehicles capable of radical shape change in flight.
Ivanco, Thomas G.   +4 more
core   +1 more source

Distributed-Flap Layout Trade Study on a Highly Flexible Common Research Model [PDF]

open access: yes
The results of a layout trade study of a full-span, trailing-edge flap system for the NASACommon Research Model (CRM) are presented. Previously developed analysis and design tools areused to determine the potential performance benefits of several flap ...
Aftosmis, Michael J.   +3 more
core   +1 more source

Active In-Flight Load Redistribution Utilizing Fiber-Optic Shape Sensing and Multiple Control Surfaces [PDF]

open access: yes
Morphing wing technologies have gained research interest in recent years as technological advancements pave the way for such innovations. A key benefit of such a morphing wing concept is the ability of the wing to transition into an optimal configuration
Martins, Benjamin L.   +2 more
core   +1 more source

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