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(Reference retrieved automatically from Web of Science through information on FAPESP grant and its corresponding number as mentioned in the publication by the authors.)

Wavepacket models for subsonic twin jets using 3D parabolized stability equations

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Author(s):
Rodriguez, Daniel [1] ; Jotkar, Mamta R. [2, 3] ; Gennaro, Elmer M. [4]
Total Authors: 3
Affiliation:
[1] Univ Fed Fluminense, Dept Mech Engn, Grad Program Mech Engn PGMEC, Lab Theoret & Appl Mech LMTA, BR-24210240 Niteroi, RJ - Brazil
[2] Univ Fed Rio de Janeiro, Ctr Tecnol, BR-21941914 Rio De Janeiro, RJ - Brazil
[3] Univ Libre Bruxelles, Nonlinear Phys Chem Unit, Brussels - Belgium
[4] Sao Paulo State Univ UNESP, Campus Sao Joao da Boa Vista, BR-13874149 Sao Joao Da Boa Vista, SP - Brazil
Total Affiliations: 4
Document type: Journal article
Source: COMPTES RENDUS MECANIQUE; v. 346, n. 10, p. 890-902, OCT 2018.
Web of Science Citations: 2
Abstract

An extension of the classical parabolized stability equations to flows strongly dependent on the two cross-stream spatial directions and weakly dependent on the streamwise one is applied to model the large-scale structures present in twin-jet configurations. The existence of these unsteady flow structures, usually referred to as wavepackets, has been demonstrated in the literature for both subsonic and supersonic round jets, along with their relation to the generation of highly directional noise emitted in the aft direction. The present study considers twin-jet configurations with different separations at high Reynolds number and subsonic conditions. The existing instability modes for the twin-jet mean flow, their dependence on the separation of the two jets, and the interaction between the wavepackets originating from the two jets is investigated here. Arising from the axisymmetric mode for single round jets, two dominant modes are found for twin jets: a varicose one, relatively insensitive to jets' proximity, but likely to be efficient in radiating noise; a sinuous one, whose amplification is strongly dependent on the jets' distance, and which can be expected to produce weaker acoustic signatures. (C) 2018 Academie des sciences. Published by Elsevier Masson SAS. All rights reserved. (AU)

FAPESP's process: 14/24782-0 - Study of the origin of unsteadiness in unforced three-dimensional laminar separation bubbles
Grantee:Elmer Mateus Gennaro
Support Opportunities: Regular Research Grants
FAPESP's process: 17/01586-0 - Instability of separated flows in aeronautical applications
Grantee:Elmer Mateus Gennaro
Support Opportunities: Regular Research Grants