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Unsteady Flow Effects in Combustor SystemsA wide variety of combustion problems, including combustion instabilities and turbulent diffusion flames, appear to involve the entrainment and deformation of laminar flames by large vortex structures in the flow field. First, some details of this process of laminar flame distortion are examined by considering the interactions of time-dependent diffusion flames with two dimensional vortices. Second, Some results on the modelling of the non-steady combustion in burners for aircraft gas turbines are given. The general aim of the work is to develop a one dimensional model applicable to the NASA-Lewis Non-Steady Combustion Rig.
Document ID
19830020961
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Subbaiah, M. V.
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1983
Publication Information
Publication: NASA. Lewis Research Center Combust. Fundamentals Res.
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
83N29232
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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