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Journal ArticleDOI

Partitioned analysis of coupled mechanical systems

TLDR
This is a tutorial article that reviews the use of partitioned analysis procedures for the analysis of coupled dynamical systems using the partitioned solution approach for multilevel decomposition aimed at massively parallel computation.
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This article is published in Computer Methods in Applied Mechanics and Engineering.The article was published on 2001-03-02. It has received 806 citations till now. The article focuses on the topics: Dynamical systems theory & State variable.

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Citations
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A three-dimensional computational analysis of fluid-structure interaction in the aortic valve

TL;DR: Results show that during systole the leaflets of the stented valve appear to be moving with the fluid in an essentially kinematical process governed by the fluid motion.
Journal ArticleDOI

Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity

TL;DR: In this paper, a second-order time-accurate and yet loosely-coupled partitioned procedure for the solution of nonlinear fluid-structure interaction (FSI) problems on moving grids is presented.
Journal ArticleDOI

An efficient solver for the fully coupled solution of large-displacement fluid–structure interaction problems

TL;DR: It is shown that block-triangular approximations of the Jacobian matrix, obtained by neglecting selected fluid–structure interaction blocks, provide good preconditioners for the solution of the linear systems with GMRES.
Journal ArticleDOI

Partitioned procedures for the transient solution of coupled aroelastic problems Part I: Model problem, theory and two-dimensional application

TL;DR: In this article, the authors present several partitioned procedures for time-integrating this focus coupled problem and discuss their merits in terms of accuracy, stability, heterogeneous computing, I/O transfers, subcycling and parallel processing.
Journal ArticleDOI

Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration

TL;DR: In this paper, a multi-point high-fidelity aerostructural optimization of a long-range wide-body transonic transport aircraft configuration is presented, where the coupled adjoint sensitivity method is used to efficiently compute gradients, enabling the use of gradient-based optimization with respect to hundreds of aerodynamic shape and structural sizing variables.
References
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Book

The finite element method

TL;DR: In this article, the methodes are numeriques and the fonction de forme reference record created on 2005-11-18, modified on 2016-08-08.

Difference methods for initial-value problems

TL;DR: In this article, differentielles and stabilite were used for differentiable transport in the context of transfert de chaleur and ondes Reference Record created on 2005-11-18, modified on 2016-08-08
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