Dynamic hydroelasticity of composite appendages with reverse-mode algorithmic differentiation

GW Ng, E Jonsson, S He, JRRA Martins - Composite Structures, 2024 - Elsevier
Composite materials enable the tailoring of load-dependent, passive, shape adaptation
because of the directional stiffness of the fibers. However, excessive flow-induced vibrations …

Bifurcation-Diagram-Free Postflutter Response Constraint for Design Optimization

C Riso, CES Cesnik, BI Epureanu - AIAA Journal, 2023 - arc.aiaa.org
This paper introduces a new metric to constrain postflutter responses of aeroelastic systems
in design optimization. The new metric aggregates the recovery rate to equilibrium for a …

High-fidelity gradient-based wing structural optimization including geometrically nonlinear flutter constraint

E Jonsson, C Riso, BB Monteiro, AC Gray… - AIAA Journal, 2023 - arc.aiaa.org
Lightweight high-aspect-ratio wings make aircraft more energy efficient thanks to their lower
induced drag. Because such wings exhibit large deflections, design optimization based on …

A Sliding-Window Matrix Pencil Method for Aeroelastic Design Optimization with Limit-Cycle Oscillation Constraints

T Golla, G Kennedy, C Riso - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
This paper presents a new approach for constraining limit-cycle oscillations in aeroelastic
design optimization. The approach builds on a gradient-oriented limit-cycle oscillation …

Adjoint-based design optimization of stability constrained systems

S He, E Jonsson, J Li, JRRA Martins - AIAA Journal, 2024 - arc.aiaa.org
A partial differential equation (PDE) constrained design optimization problem usually
optimizes a characteristic of a dynamical system around an equilibrium point. However, a …

Sliding-Window Matrix Pencil Method for Design Optimization with Limit-Cycle Oscillation Constraints

T Golla, GJ Kennedy, C Riso - AIAA Journal, 2024 - arc.aiaa.org
This paper introduces a novel approach to constrain limit-cycle oscillations in design
optimization. The approach builds upon a limit-cycle oscillation constraint that bounds the …

Data-driven airfoil shape optimization framework for enhanced flutter performance

J Jung, GX Gu - Physics of Fluids, 2024 - pubs.aip.org
This paper presents a machine learning-based airfoil shape optimization framework
designed to increase flutter resistance and reduce drag. Using the National Advisory …

Tightly Coupled Geometrically Nonlinear Structural and Aeroelastic Analysis of Flexible Wing Plate Model

W Zhao, MRH Prince, RK Kapania - AIAA SCITECH 2025 Forum, 2025 - arc.aiaa.org
This paper presents the development of a tightly coupled nonlinear aeroelastic analysis for
studying both static and dynamic aeroelastic responses of very flexible plate models. This …

High-Fidelity Aerostructural Design Optimization of Wind Turbine Rotors

M Mangano - 2024 - deepblue.lib.umich.edu
The mitigation of climate change effects through the decarbonization of the global
production system is one of the most pressing challenges of our time. Wind and solar power …

Overview of computational methods to predict flutter in aircraft

E Antimirova, J Jung, Z Zhang… - Journal of Applied …, 2024 - asmedigitalcollection.asme.org
Aeroelastic flutter is a dynamically complex phenomenon that has adverse and unstable
effects on elastic structures. It is crucial to better predict the phenomenon of flutter within the …