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contributor authorEmmanuel Motheau
contributor authorFranck Nicoud
contributor authorThierry Poinsot
date accessioned2017-05-09T00:49:49Z
date available2017-05-09T00:49:49Z
date copyrightNovember, 2012
date issued2012
identifier issn1528-8919
identifier otherJETPEZ-926033#111502_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148702
description abstractThe present study is devoted to the modeling of mean flow effects while computing thermoacoustic modes under the zero Mach number assumption. It is first recalled that the acoustic impedance modeling of a compressor or a turbine must be prescribed under an energetical form instead of the classical acoustic variables. Then we demonstrate the feasibility to take into account the coupling between acoustic and entropy waves in a zero Mach number framework to capture a family of low frequency entropic modes. The proposed approach relies on a new delayed entropy coupled boundary condition (DECBC) and proves able to capture a family of low frequency entropic mode even though no mean flow term is included in the fluctuating pressure equation.
publisherThe American Society of Mechanical Engineers (ASME)
titleUsing Boundary Conditions to Account for Mean Flow Effects in a Zero Mach Number Acoustic Solver
typeJournal Paper
journal volume134
journal issue11
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4007198
journal fristpage111502
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsMach number
keywordsAcoustics
keywordsImpedance (Electricity)
keywordsEntropy
keywordsWaves
keywordsBoundary-value problems AND Equations
treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 011
contenttypeFulltext


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