Mono-block and non-matching multi-block structured mesh adaptation based on aerodynamic functional total derivatives for RANS flow

Author:

Resmini A.12,Peter J.1,Lucor D.3

Affiliation:

1. ONERA - The French Aerospace Lab; 29, av. de la Division Leclerc 92322 Châtillon France

2. Sorbonne University; UPMC Univ Paris 06, UMR 7190, Inst Jean Le Rond dAlembert F-75005 Paris France

3. LIMSI, CNRS; Université Paris-Saclay, Campus Universitaire Bâtiment 508, Rue John von Neumann; F-91405 Orsay cedex France

Funder

Seventh Framework Programme

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference37 articles.

1. Issues in computational fluid dynamics code verification and validation;Oberkampf;AIAA Journal,1998

2. Quantification of uncertainty in computational fluid dynamics;Roache;Annual Review of Fluid Mechanics,1997

3. Sparse grids-based stochastic approximations with applications to aerodynamics sensitivity analysis;Resmini;International Journal for Numerical Methods in Engineering,2016

4. Numerics and hydrodynamics theory: towards error control in CFD;Johnson;SIAM Journal on Numerical Analysis,1995

5. Becker R Rannacher R Weighted a posteriori error control in FE methods In Proceedings of ENUMATH-97 World Scientific Publishing Heidelberg 1998

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