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Analysis of turbulent free jet hydrogen-air diffusion flames with finite chemical reaction ratesThe nonequilibrium flow field resulting from the turbulent mixing and combustion of a supersonic axisymmetric hydrogen jet in a supersonic parallel coflowing air stream is analyzed. Effective turbulent transport properties are determined using the (K-epsilon) model. The finite-rate chemistry model considers eight reactions between six chemical species, H, O, H2O, OH, O2, and H2. The governing set of nonlinear partial differential equations is solved by an implicit finite-difference procedure. Radial distributions are obtained at two downstream locations of variables such as turbulent kinetic energy, turbulent dissipation rate, turbulent scale length, and viscosity. The results show that these variables attain peak values at the axis of symmetry. Computed distributions of velocity, temperature, and mass fraction are also given. A direct analytical approach to account for the effect of species concentration fluctuations on the mean production rate of species (the phenomenon of unmixedness) is also presented. However, the use of the method does not seem justified in view of the excessive computer time required to solve the resulting system of equations.
Document ID
19780022608
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sislian, J. P.
(Toronto Univ. Ontario)
Date Acquired
September 3, 2013
Publication Date
August 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-3024
UTIAS-224
Report Number: NASA-CR-3024
Report Number: UTIAS-224
Accession Number
78N30551
Funding Number(s)
CONTRACT_GRANT: NAS1-14843
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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