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Effects of Lewis Number on Temperatures of Spherical Diffusion FlamesSpherical diffusion flames supported on a porous sphere were studied numerically and experimentally. Experiments were performed in 2.2 s and 5.2 s microgravity facilities. Numerical results were obtained from a Chemkin-based program. The program simulates flow from a porous sphere into a quiescent environment, yields both steady-state and transient results, and accounts for optically thick gas-phase radiation. The low flow velocities and long residence times in these diffusion flames lead to enhanced radiative and diffusive effects. Despite similar adiabatic flame temperatures, the measured and predicted temperatures varied by as much as 700 K. The temperature reduction correlates with flame size but characteristic flow times and, importantly, Lewis number also influence temperature. The numerical results show that the ambient gas Lewis number would have a strong effect on flame temperature if the flames were steady and nonradiating. For example, a 10% decrease in Lewis number would increase the steady-state flame temperature by 200 K. However, for these transient, radiating flames the effect of Lewis number is small. Transient predictions of flame sizes are larger than those observed in microgravity experiments. Close agreement could not be obtained without either increasing the model s thermal and mass diffusion properties by 30% or reducing mass flow rate by 25%.
Document ID
20070010443
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Santa, K. J.
(Hawaii Univ. Honolulu, HI, United States)
Sun, Z.
(Washington Univ. Saint Louis, MO, United States)
Chao, B. H.
(Hawaii Univ. Honolulu, HI, United States)
Sunderland, P. B.
(Maryland Univ. College Park, MD, United States)
Axelbaum, R. I.
(Washington Univ. Saint Louis, MO, United States)
Urban, D. L.
(NASA Glenn Research Center Cleveland, OH, United States)
Stocker, D. P.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2007
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2007-736
Report Number: AIAA Paper 2007-736
Meeting Information
Meeting: AIAA 45th Aerospace Sciences Meeting
Location: Reno, NV
Country: United States
Start Date: January 8, 2007
End Date: January 11, 2007
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNC05AA46A
CONTRACT_GRANT: NCC3-1912
CONTRACT_GRANT: NAG3-1910
CONTRACT_GRANT: NAG3-697
CONTRACT_GRANT: NCC3-696
Distribution Limits
Public
Copyright
Public Use Permitted.
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