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Non-isotropic turbulence effects on spray combustionA numerical model for the prediction of local properties of statistically stationary spray-combusting flows is evaluated by comparison with experimental data. To appraise the relative performance of turbulence models, computations were carried out by the k-epsilon model and the algebraic stress model. The present numerical results show the qualitative agreement with experimental data. In terms of overall local flow properties, the algebraic stress model improves a degree of conformity to the experimental data due to its ability to introduce the nonisotropic turbulence effects. Two swirl numbers are considered to investigate the influence of swirl on the droplet evaporation and trajectories, and the effects of droplet/turbulence interactions in flow properties. It is found that the large swirl produces a higher evaporationn rate, and more intensive turbulent mixing and burning. The discrepancies observed in the results are attributed mainly to uncertainties in the initial spray size and velocity distributions, the droplet/wall impingement interaction, the combustion model with the fast chemistry and the turbulence models dealing with the strong streamline curvature and complex interactions between the dispersed droplets and the continuous gas-phase flows.
Document ID
19910059526
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kim, Y. M.
(Alabama Univ. Huntsville, AL, United States)
Shang, H. M.
(Alabama Univ. Huntsville, AL, United States)
Chen, C. P.
(Alabama, University Huntsville, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 91-2196
Accession Number
91A44149
Funding Number(s)
CONTRACT_GRANT: NAG8-92
Distribution Limits
Public
Copyright
Other

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