[HTML][HTML] Probabilistic aeroelastic analysis of high-fidelity composite aircraft wing with manufacturing variability

M McGurk, O Stodieck, J Yuan - Composite Structures, 2024‏ - Elsevier
Safety margins of aerospace structures can be improved through altering the laminate
parameters of composite materials to increase flutter and divergence velocities. Existing …

Aeroelastic method to investigate nonlinear elastic wing structures

K Bramsiepe, T Klimmek, WR Krüger… - CEAS Aeronautical Journal, 2022‏ - Springer
Stiffness directions of wing structures are already part of the optimisation in aircraft design.
Aircraft like the A350 XWB and the Boeing 787 mainly consist of such composite material …

Wind tunnel experiment with an EPP-wing to investigate aeroelastic effects of nonlinear elastic stiffnesses

K Bramsiepe, M Braune, WR Krüger… - 33rd Congress of the …, 2022‏ - elib.dlr.de
Background: Nonlinear elastic, especially degressive, stiffnesses can reduce the wing root
bending moment for design loadcases, while the cruise flight shape remains unchanged …

Effect of Thickness Variation on the Aeroelastic Performance of Continuous Tow Sheared Structures

HJ Leitch, J Yuan, O Stodieck - AIAA SCITECH 2024 Forum, 2024‏ - arc.aiaa.org
Continuous tow shearing is a promising manufacturing technique which can produce highly
tailored steered carbon fibre laminates. This has been shown to improve the buckling …

Aeroelastic tailoring optimisation of a combat aircraft wing with tow-steered composites

A Tatar, RCM Cheung… - 19th International …, 2022‏ - research-information.bris.ac.uk
This paper investigates the possibility of employing tailored unidirectional and fibre steered
aeroelastically tailored composite lay-up techniques for a combat aircraft wing to meet …

Effects of Coupled Thickness Variation on the Aeroelastic Performance of Continuous Tow Sheared Composite Wing

H Leitch, O Stodieck, J Yuan - Available at SSRN 4786120, 2024‏ - papers.ssrn.com
Continuous tow shearing (CTS) is a promising manufacturing technique which can produce
highly tailored steered carbon fibre laminates. This has been shown to improve the buckling …

[PDF][PDF] AEROELASTIC OPTIMISATION OF A CANTILEVERED PLATE WITH LOCAL DAMPING APPLICATION

A Tatar, S Fournier, JE Cooper‏ - conf.ifasd2024.nl
This paper aims to optimise the aeroelastic performance of a cantilevered plate through the
application of a local dam** distribution. An aeroelastic model was built in MSC Nastran …