[HTML][HTML] A Comparison of Modern Metaheuristics for Multi-Objective Optimization of Transonic Aeroelasticity in a Tow-Steered Composite Wing

K Phuekpan, R Khammee, N Panagant, S Bureerat… - Aerospace, 2025 - mdpi.com
This study proposes a design procedure for the multi-objective aeroelastic optimization of a
tow-steered composite wing structure that operates at transonic speed. The aerodynamic …

Investigation of Limit Cycle Oscillations and Phase Portraits in Gfrp Based Composite Structures Embedded with Superelastic Shape Memory Alloy Wires

KS Tandel, D Raj, P Budarapu - papers.ssrn.com
Recent advancements in aerospace technology highlight the importance of high-altitude
long endurance (HALE) vehicles, emphasizing the need for high aspect ratio wing structures …

[PDF][PDF] CONTROL SURFACE SIZING AND DESIGN THROUGH INTEGRATED MDO APPROACH: ENHANCING LOAD ALLEVIATION WHILE PRESERVING …

DM Odriozola, S Marquier, J Morlier, C Gogu - conf.ifasd2024.nl
As part of ongoing efforts for cleaner and more efficient aviation, this research introduces a
novel Multidisciplinary Optimisation (MDO) strategy for the weight optimisation of High …

[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 damping distribution. An aeroelastic model was built in MSC Nastran …