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A random distribution reacting mixing layer modelA methodology for simulation of molecular mixing and the resulting velocity and temperature fields has been developed. The ideas are applied to the flow conditions present in the NASA Lewis Planar Reacting Shear Layer (PRSL) facility, and results compared to experimental data. A gaussian transverse turbulent velocity distribution is used in conjunction with a linearly increasing time scale to describe the mixing of different regions of the flow. Equilibrium reaction calculations are then performed on the mix to arrive at a new species composition and temperature. Velocities are determined through summation of momentum contributions. The analysis indicates a combustion efficiency of the order of 80 percent for the reacting mixing layer, and a turbulent Schmidt number of 2/3. The success of the model is attributed to the simulation of large-scale transport of fluid. The favorable comparison shows that a relatively quick and simple PC calculation is capable of simulating the basic flow structure in the reacting and non-reacting shear layer present in the facility given basic assumptions about turbulence properties.
Document ID
19940019079
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jones, Richard A.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-194445
NAS 1.26:194445
E-8315
Report Number: NASA-CR-194445
Report Number: NAS 1.26:194445
Report Number: E-8315
Accession Number
94N23552
Funding Number(s)
CONTRACT_GRANT: NCC3-213
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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