NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
An analysis of turbulent diffusion flame in axisymmetric jetThe kinetic theory of turbulent flow was employed to study the mixing limited combustion of hydrogen in axisymmetric jets. The integro-differential equations in two spatial and three velocity coordinates describing the combustion were reduced to a set of hyperbolic partial differential equations in the two spatial coordinates by a binodal approximation. The MacCormick's finite difference method was then employed for solution. The flame length was longer than that predicted by the flame-sheet analysis, and was found to be in general agreement with a recent experimental result. Increase of the turbulence energy and scale resulted in an enhancement of the combustion rate and, hence, in a shorter flame length. Details of the numerical method as well as of the physical findings are discussed.
Document ID
19800011171
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chung, P. M.
(Illinois Univ. Chicago, IL, United States)
Im, K. H.
(Illinois Univ. Chicago, IL, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1980
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-162884
Report Number: NASA-CR-162884
Accession Number
80N19449
Funding Number(s)
CONTRACT_GRANT: NSG-1150
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available