NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
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 Research Center 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 nonreacting shear layer present in the facility given basic assumptions about turbulence properties.
Document ID
19940024420
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, Richard A.
(Rensselaer Polytechnic Inst. Troy, NY., United States)
Marek, C. John
(NASA Lewis Research Center Cleveland, OH, United States)
Myrabo, Leik N.
(NASA Lewis Research Center Cleveland, OH, United States)
Nagamatsu, Henry T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1994
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:106517
E-8636
NASA-TM-106517
AIAA PAPER 94-3050
Report Number: NAS 1.15:106517
Report Number: E-8636
Report Number: NASA-TM-106517
Report Number: AIAA PAPER 94-3050
Meeting Information
Meeting: 30th Joint Propulsion Conference
Location: Indianapolis, IN
Country: United States
Start Date: June 27, 1994
End Date: June 29, 1994
Sponsors: AIAA, ASME, SAE, and ASEE
Accession Number
94N28923
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available