Kelvin-Helmholtz instabilities occurring at a nacelle exhaust

Julien Manera, Benoît Schiltz, Romain Leneveu, Stéphane Caro, Jonathan Jacqmot, Sjoerd Rienstra

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

26 Citations (Scopus)
2 Downloads (Pure)

Abstract

The difference of flow velocity between the free stream and the jet stream at a nacelle exhaust generates a shear layer where some hydrodynamic instabilities, called Kelvin-Helmholtz instabilities, can occur. Some instabilities occur in the shear layer in the computations with Actran/DGM a time domain code which solves the LEE equations (see,1,2 and3) but it is often difficult to conclude whether they are physical or not. This document recalls the theory on the Kelvin-Helmholtz instabilities and gives guidelines to sort out the physical and numerical instabilities. This methodology is put into practice on concrete cases studied in the frame of the TURNEX project.

Original languageEnglish
Title of host publication14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
Place of PublicationReston
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages18
ISBN (Print)9781563479397
DOIs
Publication statusPublished - 1 Dec 2008
Event14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference) - Vancouver, BC, Canada
Duration: 5 May 20087 May 2008

Conference

Conference14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
Country/TerritoryCanada
CityVancouver, BC
Period5/05/087/05/08

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