Assessment of CFD Predictive Capability for Aeronautical Applications

N. Thouault (), F. Vogel (), C. Breitsamter and N. A. Adams
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N. Thouault: Technische Universität München, Lehrstuhl für Aerodynamik
F. Vogel: Technische Universität München, Lehrstuhl für Aerodynamik
C. Breitsamter: Technische Universität München, Lehrstuhl für Aerodynamik
N. A. Adams: Technische Universität München, Lehrstuhl für Aerodynamik

A chapter in High Performance Computing in Science and Engineering, Garching/Munich 2009, 2010, pp 121-132 from Springer

Abstract: Abstract The present work focuses on assessing the predictive capabilities of state-of-the-art Computational Fluid Dynamics methods for aerospace engineering appplications by comparison with experimental data. Two relevant cases are tested: a generic fan-in-wing configuration and a helicopter fuselage. Unsteady Reynolds Averaged Navier Stokes and Scale-Adaptive Simulations are carried out to predict the flow physics of such complex geometry arrangements. The simulation results show a satisfactory agreement with a wide range of experimental data.

Keywords: Particle Image Velocimetry; Wind Tunnel; Computational Fluid Dynamics Method; Aeronautical Application; Root Chord (search for similar items in EconPapers)
Date: 2010
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Persistent link: https://EconPapers.repec.org/RePEc:spr:sprchp:978-3-642-13872-0_11

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DOI: 10.1007/978-3-642-13872-0_11

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