BI Epureanu - Journal of fluids and structures, 2003 - Elsevier
The unsteady flow created by a cascade of oscillating airfoils is investigated. A frequency- domain model is constructed and the proper orthogonal decomposition technique is applied …
In this study, the modeling of the compressible pressure field on the RAE 2822 airfoil using deep learning (DL) is investigated. The objective is to generate, at low cost, the complete …
Reduced order models (ROM) are commonly employed to solve parametric problems and to devise inexpensive response surfaces to evaluate quantities of interest in real-time. There …
K Decker, HD Schwartz, D Mavris - AIAA Aviation 2020 Forum, 2020 - arc.aiaa.org
This study presents a methodology for the use of parametric Reduced Order Modeling (ROM) techniques to generate predictive models of hypersonic aerodynamic flow fields. The …
Y Hou, C Liu, H Hu - Computer Methods in Applied Mechanics and …, 2020 - Elsevier
Nonlinear finite element methods such as isogeometric analysis and absolute nodal coordinate formulation can be applied to modeling the flexible multibody systems (FMBS) …
This study presents the development of a methodology for the construction of data-driven, parametric, multifidelity reduced-order models to emulate aerodynamic flowfields with …
In this paper, we put forth an evolve-then-correct reduced order modeling approach that combines intrusive and nonintrusive models to take hidden physical processes into account …
PS Beran, DJ Lucia, CL Pettit - Journal of Fluids and Structures, 2004 - Elsevier
Limit-cycle oscillations (LCOs) of a nonlinear panel in supersonic flow are computed using a reduced-order aeroelastic model. Panel dynamics are governed by the large-deflection …