Reference : Using Proper Orthogonal Decomposition Methods for Comparing CFD Results to Experimental ...
Scientific congresses and symposiums : Paper published in a book
Engineering, computing & technology : Aerospace & aeronautics engineering
http://hdl.handle.net/2268/131610
Using Proper Orthogonal Decomposition Methods for Comparing CFD Results to Experimental Measurements
English
Andrianne, Thomas mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Département d'aérospatiale et mécanique >]
Guissart, Amandine mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Modélisation et contrôle des écoulements turbulents >]
Terrapon, Vincent mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Modélisation et contrôle des écoulements turbulents >]
Dimitriadis, Grigorios mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale >]
3-Oct-2012
Proceedings of the 5th Symposium on Integrating CFD and Experiments in Aerodynamics (Integration 2012)
12
No
International
5th Symposium on Integrating CFD and Experiments in Aerodynamics (Integration 2012)
from 02-10-2012 to 05-10-2012
JAXA
Chofu Aerospace Center, Tokyo
Japan
[en] Unsteady aerodynamics ; PIV ; CFD ; Proper Orthogonal Decomposition ; Wind tunnel ; uRANS ; OpenFOAM
[en] This work presents a method for quantitative comparison of numerical results to experimental measurements. It is based on the concept of Proper Orthogonal Decomposition. This technique is selected in order to compare the unsteady aerodynamic flows around static and oscillating bodies obtained from wind tunnel testing and numerical simulations. Two dimensional Time-resolved Particle Image Velocimetry measurements are carried out on the upper surface a 4:1 rectangular cylinder. Simulations are performed using unsteady Reynolds-Averaged Navier-Stokes and an unsteady Discrete Vortex Method. It is demonstrated that the proposed technique is a good preliminary step for comparing the main characteristics of unsteady aerodynamic data.
Researchers ; Professionals ; Students
http://hdl.handle.net/2268/131610

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