Numerical/experimental simulation of exhaust jet mixing in wake vortex

S. Brunet, F. Garnier, L. Jacquin

Research output: Contribution to conferencePaperpeer-review

Abstract

This study is a contribution to the understanding and modeling of engine jet dispersion of an aircraft in cruise condition. One presents a three-dimensional direct numerical simulation (DNS) of the interaction between jets and a vortex wake compared to the results of a wind tunnel experiment. The experimental data described herein comprises velocity fields measured by a Laser Doppler Velocimeter (LDV) and mean temperature fields delivered by thermocouples1. The DNS is in qualitative agreement with the experiment but inspection shows departures caused by an underestimation of the jet mixing during the first phases of the jet development.

Original languageEnglish
Publication statusPublished - 1 Jan 1999
Externally publishedYes
Event30th Fluid Dynamics Conference, 1999 - Norfolk, United States
Duration: 28 Jun 19991 Jul 1999

Conference

Conference30th Fluid Dynamics Conference, 1999
Country/TerritoryUnited States
CityNorfolk
Period28/06/991/07/99

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