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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. The rapid growth in scientific knowledge and research necessitates the consolidation of the latest research and technological ...
Najmi J   +4 more
europepmc   +4 more sources

Wind Tunnel Measurement Systems for Unsteady Aerodynamic Forces on Bluff Bodies: Review and New Perspective [PDF]

open access: yesSensors, 2020
Wind tunnel tests have become one of the most effective ways to evaluate aerodynamics and aeroelasticity in bluff bodies. This paper has firstly overviewed the development of conventional wind tunnel test techniques, including high frequency base balance
Zengshun Chen   +3 more
doaj   +2 more sources

State of the art in the aeroelasticity of wind turbine blades: Aeroelastic modelling [PDF]

open access: yesRenewable and Sustainable Energy Reviews, 2016
With the continuous increasing size and flexibility of large wind turbine blades, aeroelasticity has been becoming a significant subject for wind turbine blade design. There have been some examples of commercially developed wind turbines experiencing aeroelastic instability problems in the last decade, which spokes for the necessity of aeroelastic ...
Lin Wang   +2 more
exaly   +3 more sources

Potential Estimation of Load Alleviation and Future Technologies in Reducing Aircraft Structural Mass

open access: yesAerospace, 2022
In recent years, load alleviation technologies have been more widely used in transport aircraft. For aircraft already in service, load alleviation can contribute in extending the fatigue life, or enable small configurational changes.
Vega Handojo   +4 more
doaj   +1 more source

Nonlinear Aeroelastic Simulations and Stability Analysis of the Pazy Wing Aeroelastic Benchmark

open access: yesAerospace, 2021
The Pazy wing aeroelastic benchmark is a highly flexible wind tunnel model investigated in the Large Deflection Working Group as part of the Third Aeroelastic Prediction Workshop.
Jonathan Hilger, Markus Raimund Ritter
doaj   +1 more source

Effect of Aerodynamic Damping Approximations on Aeroelastic Eigensensitivities

open access: yesAerospace, 2022
Aeroelastic sensitivities for the flutter solution are a crucial component of the multi-disciplinary optimization methods employed in modern aircraft design.
Christoph Kaiser, David Quero
doaj   +1 more source

Development of aeroelastic modeling and analysis for wing camber morphing technology

open access: yesHangkong gongcheng jinzhan, 2023
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

Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device [PDF]

open access: yesJournal of Aircraft, 2020
A recent consideration in aircraft design is the use of folding wingtips, with the aim of enabling higher-aspect-ratio aircraft with less induced drag but also meeting airport gate limitations.
Castrichini A.   +5 more
openaire   +5 more sources

Influence of Fluid Viscosity and Compressibility on Nonlinearities in Generalized Aerodynamic Forces for T-Tail Flutter

open access: yesAerospace, 2022
The numerical assessment of T-tail flutter requires a nonlinear description of the structural deformations when the unsteady aerodynamic forces comprise terms from lifting surface roll motion.
Dominik Schäfer
doaj   +1 more source

Parametric Modeling of a Long-Range Aircraft under Consideration of Engine-Wing Integration

open access: yesAerospace, 2020
The purpose of this paper is to investigate the influence of the engine position and mass as well as the pylon stiffness on the aeroelastic stability of a long-range wide-body transport aircraft. As reference configuration, DLR’s (German Aerospace Center/
Matthias Schulze   +2 more
doaj   +1 more source

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