Results 1 to 10 of about 133 (124)

Aeroelastic tailoring for aerospace applications [PDF]

open access: yesHeliyon, 2023
This study presents a brief account of the seminal works on aeroelastic tailoring for aerospace applications. Tailoring using advanced composites is a revolutionary process in the ever-evolving realm of aerospace design.
Asad Hameed   +2 more
exaly   +6 more sources

Application of Aeroelastic Tailoring for Load Alleviation on a Flying Demonstrator Wing

open access: yesAerospace, 2022
This article presents the application of aeroelastic tailoring in the design of wings for a flying demonstrator, as well as the validation of the design methodology with flight test results.
Jurij Sodja   +2 more
exaly   +3 more sources

Aeroelastic Tailoring of the Next Generation Civil Tiltrotor Technological Demonstrator Composite Wing

open access: yesAerospace, 2022
The tiltrotor wing structure is one of the most critical and heavily investigated structures in design due to the fundamental need to consider the interactions between the wing, pylon, and rotor systems to achieve aircraft aeroelastic stability.
Aniello Daniele Marano   +2 more
exaly   +3 more sources

Aeroelastic tailoring using crenellated skins-modelling and experiment [PDF]

open access: yesAdvances in Aircraft and Spacecraft Science, 2017
Aeroelastic performance controls wing shape in flight and its behaviour under manoeuvre and gust loads. Controlling the wing’s aeroelastic performance can therefore offer weight and fuel savings. In this paper, the rib orientation and the crenellated skin concept are used to control wing deformation under aerodynamic load. The impact of varying the rib/
Paul Weaver
exaly   +3 more sources

Aeroelastic tailoring of a plate wing with functionally graded materials [PDF]

open access: yesJournal of Fluids and Structures, 2014
This work explores the use of functionally graded materials for the aeroelastic tailoring of a metallic cantilevered plate-like wing. Pareto trade-off curves between dynamic stability (flutter) and static aeroelastic stresses are obtained for a variety of grading strategies.
Peter Dunning, H Alicia Kim
exaly   +3 more sources

The Effect of Laminated Layers on the Flutter Speed of Composite Wing

open access: yesJournal of Engineering, 2023
The paper presents an investigation to the flutter speed of composite wing for different ply orientation. Structurally the composite wing was idealized as a composite beam load carrying structure. Theodorsen’s expression was used to get the 2- dimension
Ahmed Abd Al-Hussain Ali   +1 more
doaj   +1 more source

Structural design and modal behaviors analysis of a new swept baffled inflatable wing

open access: yesDefence Technology, 2023
Inflatable wing has significant application value in the design of loitering munitions because of its advantages such as lightweight and foldability. However, due to the flexible characteristics, aeroelastic behaviors of inflatable wings such as flutter ...
Nuo Ma, Li Liu, Fanmin Meng, Junhui Meng
doaj   +1 more source

Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm

open access: yesInternational Journal of Aerospace Engineering, 2022
This work investigates thermal aeroelastic tailoring of a laminated composite panel with a lamination parameter-based method. Equivalent membrane and bending coefficients of thermal expansions for symmetric laminated panel are derived and represented ...
Peng Jin, Qihao Zheng, Wei Wei
doaj   +1 more source

The Impact of Bend–Twist Coupling on Structural Characteristics and Flutter Limit of Ultra-Long Flexible Wind Turbine Composite Blades

open access: yesEnergies, 2023
Flutter is an instability phenomenon that can occur in wind turbine blades due to fluid–structure interaction, particularly for longer and more flexible blades.
Bei Li   +4 more
doaj   +1 more source

Effect of Aeroelastic Tailoring Design on Wing Mode

open access: yesInternational Journal of Aerospace Engineering, 2023
In this paper, in order to clarify the influence of structural parameters of laminates on the modal characteristics of high-aspect-ratio wings under prestress, the CFD/CSD coupling method was used to study the modal characteristics of nonlinear ...
Yajuan He   +5 more
doaj   +1 more source

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