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A model of concurrent flow flame spread over a thin solid fuelA numerical model is developed to examine laminar flame spread and extinction over a thin solid fuel in lowspeed concurrent flows. The model provides a more precise fluid-mechanical description of the flame by incorporating an elliptic treatment of the upstream flame stabilization zone near the fuel burnout point. Parabolic equations are used to treat the downstream flame, which has a higher flow Reynolds number. The parabolic and elliptic regions are coupled smoothly by an appropriate matching of boundary conditions. The solid phase consists of an energy equation with surface radiative loss and a surface pyrolysis relation. Steady spread with constant flame and pyrolysis lengths is found possible for thin fuels and this facilitates the adoption of a moving coordinate system attached to the flame with the flame spread rate being an eigen value. Calculations are performed in purely forced flow in a range of velocities which are lower than those induced in a normal gravity buoyant environment. Both quenching and blowoff extinction are observed. The results show that as flow velocity or oxygen percentage is reduced, the flame spread rate, the pyrolysis length, and the flame length all decrease, as expected. The flame standoff distance from the solid and the reaction zone thickness, however, first increase with decreasing flow velocity, but eventually decrease very near the quenching extinction limit. The short, diffuse flames observed at low flow velocities and oxygen levels are consistent with available experimental data. The maximum flame temperature decreases slowly at first as flow velocity is reduced, then falls more steeply close to the quenching extinction limit. Low velocity quenching occurs as a result of heat loss. At low velocities, surface radiative loss becomes a significant fraction of the total combustion heat release. In addition, the shorter flame length causes an increase in the fraction of conduction downstream compared to conduction to the fuel. These heat losses lead to lower flame temperatures, and ultimately, extinction. This extinction mechanism differs from that of blowoff, where the flame is unable to be stabilized due to the high flow velocity.
Document ID
19930015757
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ferkul, Paul V.
(Case Western Reserve Univ. Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1993
Subject Category
Materials Processing
Report/Patent Number
NASA-CR-191111
E-7726
NAS 1.26:191111
Report Number: NASA-CR-191111
Report Number: E-7726
Report Number: NAS 1.26:191111
Accession Number
93N24946
Funding Number(s)
CONTRACT_GRANT: NAG3-1046
PROJECT: RTOP 674-22-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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