Frequency lock-in in pitch–heave stall flutter
D Poirel, L Goyaniuk, A Benaissa - Journal of Fluids and Structures, 2018 - Elsevier
Coupled pitch–heave oscillations of a rigid but elastically mounted NACA0012 wing are
experimentally investigated in a range of airspeeds corresponding to transitional Reynolds …
experimentally investigated in a range of airspeeds corresponding to transitional Reynolds …
Combined selection of the dynamic model and modeling error in nonlinear aeroelastic systems using Bayesian Inference
We report a Bayesian framework for concurrent selection of physics-based models and
(modeling) error models. We investigate the use of colored noise to capture the mismatch …
(modeling) error models. We investigate the use of colored noise to capture the mismatch …
Bayesian model selection using automatic relevance determination for nonlinear dynamical systems
Bayesian model selection is augmented with automatic relevance determination (ARD) to
perform model reduction of complex dynamical systems modelled by nonlinear, stochastic …
perform model reduction of complex dynamical systems modelled by nonlinear, stochastic …
Comprehensive compartmental model and calibration algorithm for the study of clinical implications of the population-level spread of COVID-19: a study protocol
Introduction The complex dynamics of the coronavirus disease 2019 (COVID-19) pandemic
has made obtaining reliable long-term forecasts of the disease progression difficult. Simple …
has made obtaining reliable long-term forecasts of the disease progression difficult. Simple …
Nonlinear sparse Bayesian learning for physics-based models
This paper addresses the issue of overfitting while calibrating unknown parameters of over-
parameterized physics-based models with noisy and incomplete observations. A semi …
parameterized physics-based models with noisy and incomplete observations. A semi …
Effect of Hopf-Hopf bifurcation on the post-flutter behavior of a three-degree-of-freedom airfoil
X Wu, G Li, Y Yue - Aerospace Science and Technology, 2024 - Elsevier
The post-flutter dynamics of a three-degree-of-freedom nonlinear airfoil with unsteady
aerodynamics are investigated based on the Hopf-Hopf bifurcation theory. Many prior works …
aerodynamics are investigated based on the Hopf-Hopf bifurcation theory. Many prior works …
Amplitude annihilation in wake-influenced aeroelastic limit-cycle oscillations
BA Kirschmeier, Z Gianikos, A Gopalarathnam… - AIAA Journal, 2020 - arc.aiaa.org
This paper investigates the dynamics of a pitching and heaving aeroelastic wing undergoing
large-amplitude limit-cycle oscillations influenced by a vortical wake from an upstream …
large-amplitude limit-cycle oscillations influenced by a vortical wake from an upstream …
Encoding nonlinear and unsteady aerodynamics of limit cycle oscillations using nonlinear sparse Bayesian learning
This article investigates the applicability of a recently proposed, nonlinear sparse Bayesian
learning (NSBL) algorithm to identify and estimate the complex aerodynamics of limit cycle …
learning (NSBL) algorithm to identify and estimate the complex aerodynamics of limit cycle …
Hysteresis behavior and generalized Hopf bifurcation in a three-degrees-of-freedom aeroelastic system with concentrated nonlinearities
X Wu, G Li, Y Yue - Communications in Nonlinear Science and Numerical …, 2024 - Elsevier
A three-degrees-of-freedom aeroelastic system with concentrated structural nonlinearities is
considered. The aerodynamic loads in the model are simulated by using unsteady …
considered. The aerodynamic loads in the model are simulated by using unsteady …
Aeroelastic oscillations of a pitching flexible wing with structural geometric nonlinearities: Theory and numerical simulation
This paper focuses on the derivation of an analytical model of the aeroelastic dynamics of an
elastically mounted flexible wing. The equations of motion obtained serve to help …
elastically mounted flexible wing. The equations of motion obtained serve to help …