2009•47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace ExpositionRequires access

Application of Advanced CFD Tools for High Reynolds Number Testing

Stefan Melber-Wilkending, Georg Wichmann

Abstract

Numerical simulations of the DLR F11 high lift half model in landing configuration in the test section of the ETW wind tunnel have been carried out with the unstructured CFD code DLR TAU. The numerical results are compared to measurements of the cryogenic wind tunnel ETW performed within the EU project FLIRET. The tests have been conducted with three different peniche heights of the F11 model to determine the influence of the so called half model mounting effects on the aerodynamic characteristics of model flow. Based on the numerical simulation of the half model tests the peniche effects and the wind tunnel flow itself are analyzed. The capability of the used CFD code for high Reynolds number testing is demonstrated.

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Key concepts: Computational fluid dynamics, Reynolds number, Computer science, Mechanics, Engineering, Aerospace engineering, Physics, Turbulence