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RSM-RANS Computation of Aircraft Engine Intake U-Ducts

descriptionPublicationkeyboard_double_arrow_right Conference object , Other literature type 14 Jun 2009Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:39th AIAA Fluid Dynamics Conference

Authors: G.A. Gerolymos; S. Joly; M. Mallet; I. Vallet;

doi: 10.2514/6.2009-4161

RSM-RANS Computation of Aircraft Engine Intake U-Ducts

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Abstract

The purpose of the present paper is the assessment of wall-topology free second-moment and k " closures for the computation of flows in aircraft engine intake U-duct configurations. It is shown that the wall-normal-free Reynolds-stress model with an optimized redistribution-term closure is in good agreement with experiment, largely improving upon linear 2-equation closure.

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12 Research products, page 1 of 2

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