Stability analysis of reacting wakes: Flow and density asymmetry effects

Benjamin Emerson, Swapnil Jagtap, Michael W. Renfro, Baki M. Cetegen, Tim Lieuwen

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

4 Scopus citations

Abstract

This paper explores the hydrodynamic stability of bluff body wakes with non-uniform mean density, and with asymmetric mean density and velocity profiles. This work is motivated by recent experimental bluff body combustor studies by Tuttle et al. [1], which investigated reacting wakes with equivalence ratio stratification, and hence asymmetry in the base flow density profiles. They showed that highly stratified cases exhibited strong, narrowband oscillations, suggestive of global hydrodynamic instability. In this paper, we present a hydrodynamic stability analysis for non-uniform density wakes that includes base flow asymmetry. The results show that increasing the degree of base density asymmetry is generally a destabilizing effect, and that increasing base velocity asymmetry tends to be stabilizing. Furthermore, we show that increasing base density asymmetry slightly decreases the absolute frequency, and that increasing the base velocity asymmetry slightly increases the absolute frequency. In addition, we show that increasing the degree of base density asymmetry distorts the most absolutely unstable hydrodynamic mode from its nominally sinuous structure. This distorted mode exhibits higher amplitude pressure and velocity oscillations near the flame with the lower density jump, than near the flame with the higher density jump. This would then be anticipated to lead to strongly non-symmetric amplitudes of flame flapping, with much stronger flame flapping on the side with lower density ratio. These predictions are shown to be consistent with the experimental data measured by Tuttle et al. [1]. These comparisons support the analytical predictions that increased base density is destabilizing, and that hydrodynamic velocity fluctuation amplitudes should be greatest at the flame with the lowest density jump.

Original languageEnglish
Title of host publication53rd AIAA Aerospace Sciences Meeting
DOIs
StatePublished - 2015
Event53rd AIAA Aerospace Sciences Meeting, 2015 - Kissimmee, United States
Duration: Jan 5 2015Jan 9 2015

Publication series

Name53rd AIAA Aerospace Sciences Meeting

Conference

Conference53rd AIAA Aerospace Sciences Meeting, 2015
Country/TerritoryUnited States
CityKissimmee
Period1/5/151/9/15

Bibliographical note

Publisher Copyright:
© 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

ASJC Scopus subject areas

  • Aerospace Engineering

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