David Amsallem, Daniel Neumann, Youngsoo Choi, Charbel Farhat
Published 2015-06-23Version 1
An iterative, CFD-based approach for aeroelastic computations in the frequency domain is presented. The method relies on a linearized formulation of the aeroelastic problem and a fixed-point iteration approach and enables the computation of the eigenproperties of each of the wet aeroelastic eigenmodes. Numerical experiments on the aeroelastic analysis and design optimization of two wing configurations illustrate the capability of the method for the fast and accurate aeroelastic analysis of aircraft configurations and its advantage over classical time-domain approaches.
Implementation of the Critical Wave Groups Method with Computational Fluid Dynamics and Neural Networks
On the comparison between pre- and post-surgery nasal anatomies via computational fluid dynamics
Application of Video-to-Video Translation Networks to Computational Fluid Dynamics
![QR code for arXiv:1506.07441 [physics.flu-dyn]](http://oss.arxitics.com/images/favicon.svg)