High Performance Computing Towards Silent Flows

E. Gröschel (), D. König (), S. Koh, W. Schröder and M. Meinke
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E. Gröschel: RWTH Aachen University, Institute of Aerodynamics
D. König: RWTH Aachen University, Institute of Aerodynamics
S. Koh: RWTH Aachen University, Institute of Aerodynamics
W. Schröder: RWTH Aachen University, Institute of Aerodynamics
M. Meinke: RWTH Aachen University, Institute of Aerodynamics

A chapter in High Performance Computing on Vector Systems 2007, 2008, pp 115-135 from Springer

Abstract: Abstract The flow field and the acoustic field of various jet flows and a high-lift configuration consisting of a deployed slat and a main wing are numerically analyzed. The flow data, which are computed via large-eddy simulations (LES), provide the distributions being plugged in the source terms of the acoustic perturbation equations (APE) to compute the acoustic near field. The investigation emphasizes the core flow to have a major impact on the radiated jet noise. In particular the effect of heating the inner stream generates substantial noise to the sideline of the jet, whereas the Lamb vector is the dominant noise source for the downstream noise. Furthermore, the analysis of the airframe noise shows the interaction of the shear layer of the slat trailing edge and the slat gap flow to generate higher vorticity than the main airfoil trailing edge shear layer. Thus, the slat gap is the more dominant noise region for an airport approaching aircraft.

Keywords: Shear Layer; High Performance Computing; Suction Side; Main Wing; Acoustic Simulation (search for similar items in EconPapers)
Date: 2008
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DOI: 10.1007/978-3-540-74384-2_10

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