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Validating a Monotonically-Integrated Large Eddy Simulation Code for Subsonic Jet Acoustics
Author(s) -
Daniel Ingraham,
James Bridges
Publication year - 2017
Publication title -
54th aiaa aerospace sciences meeting
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2017-0456
Subject(s) - solver , polygon mesh , jet (fluid) , jet noise , code (set theory) , point (geometry) , large eddy simulation , set (abstract data type) , noise (video) , turbulence , physics , computer science , acoustics , mechanics , mathematics , geometry , mathematical optimization , artificial intelligence , image (mathematics) , programming language
The results of subsonic jet validation cases for the Naval Research Lab's Jet Engine Noise REduction (JENRE) code are reported. Two set points from the Tanna matrix, set point 3 (Ma = 0.5, unheated) and set point 7 (Ma = 0.9, unheated) are attempted on three different meshes. After a brief discussion of the JENRE code and the meshes constructed for this work, the turbulent statistics for the axial velocity are presented and compared to experimental data, with favorable results. Preliminary simulations for set point 23 (Ma = 0.5, Tj=T1 = 1.764) on one of the meshes are also described. Finally, the proposed configuration for the farfield noise prediction with JENRE's Ffowcs-Williams Hawking solver are detailed.

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