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Turbulent Premixed Flame Propagation in MicrogravityThe structure and propagation characteristics of turbulent premixed flames have been investigated for some time. For example, the turbulent flame speed has been typically estimated m terms of the laminar flame speed SL and the local turbulence intensity u. However, the exact form of the functional relation: uT/SL = f(SL,u ) has not yet been determined although various models have been proposed. A key reason for this uncertainty is the inability to experimentally resolve all scales of motion that could contribute to the wrinkling of the premixed flame and hence, to an increase the effective burn speed. In a typical high Reynolds number flow, the small scales are impossible to resolve m an experiment (e.g., using LDV). However, turbulent fluctuations at the small scales (e.g., Kolmogorov scale) could be resolved if the Reynolds number is reduced (for example, by reducing the flow velocity). A flow field that provides sustained turbulent flow in a relatively low Reynolds number is Couette flow. It has been shown m past studies that stationmy turbulent Couette flow could be achieved at Reynolds number as low as 1800. Once combustion is included, however, the large-scale turbulent stresses responsible for momentum transport can be overwhelmed by the buoyant stresses in lg. Since this phenomenon is not present in realistic high Reynolds number devices, a microgravity environment is required to suppress the buoyancy effects while still maintaining reasonable operating pressure, temperature and observable scales at all sizes.
Document ID
19970020572
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
S Menon
(Georgia Institute of Technology Atlanta, United States)
M Disseau
(Georgia Institute of Technology Atlanta, United States)
V K Chakravarthy
(Georgia Institute of Technology Atlanta, United States)
J Jagoda
(Georgia Institute of Technology Atlanta, United States)
Date Acquired
August 17, 2013
Publication Date
May 1, 1997
Publication Information
Publication: Fourth International Microgravity Combustion Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Materials Processing
Report/Patent Number
NASA-CP-10194
Meeting Information
Meeting: Fourth International Microgravity Combustion Workshop
Location: Cleveland, OH
Country: US
Start Date: May 19, 1997
End Date: May 21, 1997
Sponsors: National Aeronautics and Space Administration
Accession Number
97N21845
Funding Number(s)
CONTRACT_GRANT: NAG3-1610
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
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