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Turbulent Premixed Flames in MicrogravityThe experimental cold-flow facility is now full operational and is currently being used to obtain baseline turbulence data in a Couette flow. The baseline turbulence data is necessary to confirm the capability of the chosen device to generate and maintain the required turbulence intensity. Subsequent reacting flow studies will assume that a similar turbulent flow field exists ahead of the premixed flame. Some modifications and refinements had to be made to enable accurate measurements. It consists of two rollers, one (driven by a motor) which drives a continuous belt and four smaller rollers used to set the belt spacing and tension to minimize belt flutter. The entire assemble is enclosed in a structure that has the dimensions to enable future drop tower experiments of the hot facility. All critical dimensions are the same as the original plans except for the pulley ratio which has been changed to enable a wider operating regime in terms of the Reynolds number. With the current setup, Reynolds numbers as low as 100 and as high as 14,000 can be achieved. This is because the in-between belt spacing can be varied from 1 cm to 7.6 cm, and the belt speed can be accurately varied from .15 m/sec to 3.1 m/sec.
Document ID
19960021019
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Menon, Suresh
(Georgia Inst. of Tech. Atlanta,GA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Subject Category
Materials Processing
Report/Patent Number
NASA-CR-200888
NAS 1.26:200888
Report Number: NASA-CR-200888
Report Number: NAS 1.26:200888
Accession Number
96N24511
Funding Number(s)
CONTRACT_GRANT: NAG3-1610
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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