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contributor authorDilip Prasad
contributor authorJinzhang Feng
date accessioned2017-05-09T00:14:39Z
date available2017-05-09T00:14:39Z
date copyrightOctober, 2004
date issued2004
identifier issn0889-504X
identifier otherJOTUEI-28715#637_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130965
description abstractA numerical method is developed for transient linear analysis of quasi-one-dimensional thermoacoustic systems, with emphasis on stability properties. This approach incorporates the effects of mean flow variation as well as self-excited sources such as the unsteady heat release across a flame. Working in the frequency domain, the perturbation field is represented as a superposition of local wave modes, which enables the linearized equations to be integrated in space. The problem formulation is completed by specifying appropriate boundary conditions. Here, we consider impedance boundary conditions as well as those relevant to choked and shocked flows. For choked flows, the boundary condition follows from the requirement that perturbations remain regular at the sonic point, while the boundary conditions applicable at a normal shock are obtained from the shock jump conditions. The numerical implementation of the proposed formulation is described for the system eigenvalue problem, where the natural modes are sought. The scheme is validated by comparison with analytical and numerical solutions.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermoacoustic Stability of Quasi-One-Dimensional Flows–Part I: Analytical and Numerical Formulation
typeJournal Paper
journal volume126
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1791288
journal fristpage637
journal lastpage644
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsEigenvalues
keywordsEquations
keywordsBoundary-value problems
keywordsStability AND Shock (Mechanics)
treeJournal of Turbomachinery:;2004:;volume( 126 ):;issue: 004
contenttypeFulltext


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