Abstract

Certain two and three dimensional numerical solutions to the adjoint Euler equations have a value at and near the surface of wings and airfoils that depends strongly on the mesh density and which does not converge as the mesh is refined. The purpose of this paper is to characterize this problem and offer insights as to the possible explanation of this unusual behavior.

Full document

The PDF file did not load properly or your web browser does not support viewing PDF files. Download directly to your device: Download PDF document
Back to Top
GET PDF

Document information

Published on 11/03/21
Submitted on 11/03/21

Volume 1300 - Inverse Problems, Optimization and Design, 2021
DOI: 10.23967/wccm-eccomas.2020.258
Licence: CC BY-NC-SA license

Document Score

0

Views 60
Recommendations 0

Share this document

claim authorship

Are you one of the authors of this document?