| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8058632 | Aerospace Science and Technology | 2016 | 14 Pages |
Abstract
The method is calibrated and illustrated using a three-dimensional toy model database that is obtained by discretizing a transcendental function. The performance of the method is tested on three aerodynamic databases for the flow past a wing, one obtained by a semi-analytical method, and two resulting from computational fluid dynamics.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Ana I. Moreno, Artur A. Jarzabek, José M. Perales, José M. Vega,