Volterra-series-based nonlinear system modeling and its engineering applications: A state-of-the-art review

CM Cheng, ZK Peng, WM Zhang, G Meng - Mechanical Systems and Signal …, 2017 - Elsevier
Nonlinear problems have drawn great interest and extensive attention from engineers,
physicists and mathematicians and many other scientists because most real systems are …

On the generation of flight dynamics aerodynamic tables by computational fluid dynamics

A Da Ronch, M Ghoreyshi, KJ Badcock - Progress in Aerospace Sciences, 2011 - Elsevier
An approach for the generation of aerodynamic tables using computational fluid dynamics is
discussed. For aircraft flight dynamics, forces and moments are often tabulated in multi …

Optimal sparsity in nonlinear nonparametric reduced order models for transonic aeroelastic systems

M Candon, E Hale, A Delgado-Gutiérrez, P Marzocca… - AIAA Journal, 2024 - arc.aiaa.org
Machine learning and artificial intelligence algorithms typically require a large amount of
data for training. This means that for nonlinear aeroelastic applications, where small training …

Parameterization of nonlinear aeroelastic reduced order models via direct interpolation of Taylor partial derivatives

M Candon, E Hale, M Balajewicz… - Nonlinear …, 2024 - Springer
The identification of optimally sparse Taylor partial derivatives presents a new opportunity in
efficient nonlinear model reduction for complex aeroelastic systems. Unfortunately, for this …

Evaluation of linear, inviscid, viscous, and reduced-order modelling aeroelastic solutions of the AGARD 445.6 wing using root locus analysis

WA Silva, P Chwalowski, B Perry III - International Journal of …, 2014 - Taylor & Francis
Reduced-order modelling (ROM) methods are applied to the Computational Fluid Dynamics
(CFD)-based aeroelastic analysis of the AGARD 445.6 wing in order to gain insight …

Reduced-order modeling of unsteady aerodynamics across multiple mach regimes

T Sku**s, CES Cesnik - Journal of Aircraft, 2014 - arc.aiaa.org
A reduced-order model for unsteady aerodynamic calculations across a range of Mach
regimes based on linear convolution and a nonlinear correction factor is developed …

Transonic aerodynamic load modeling of X-31 aircraft pitching motions

M Ghoreyshi, RM Cummings, AD Ronch, KJ Badcock - AIAA journal, 2013 - arc.aiaa.org
The generation of reduced-order models for computing the unsteady and nonlinear
aerodynamic loads on an aircraft from pitching motions in the transonic speed range is …

Aeroelastic optimization design of composite materials blade based on RBF/ROM and CCA reliability analysis

B Zhang, Q Wang, X Liu, L Zu, H Yuan - Composite Structures, 2022 - Elsevier
Carbon fiber composites have been widely used in rotor blades due to their excellent
mechanical performance, lightweight and designing flexibility. The modern fluid–structure …

Efficient Transonic Aeroelastic Model Reduction Using Optimized Sparse Multi-Input Polynomial Functionals

M Candon, M Balajewicz, A Delgado-Gutierrez… - arxiv preprint arxiv …, 2024 - arxiv.org
Nonlinear aeroelastic reduced-order models (ROMs) based on machine learning or artificial
intelligence algorithms can be complex and computationally demanding to train, meaning …

ADVANCES AND PROSPECTS OF THE REDUCED ORDER\\MODEL FOR UNSTEADY FLOW AND ITS APPLICATION

G Chen, Y Li - 力学进展, 2011 - lxjz.cstam.org.cn
With the development of the large scale numerical simulation, computational fluid dynamics
and computational solid mechanics couplesimulation becomes the powerful accurate tool in …