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Deposition of Na2SO4 from salt-seeded combustion gases of a high velocity burner rigThe mechanism of deposition of Na2SO4 was studied under controlled laboratory conditions and the results have been compared to a recently developed comprehensive theory of vapor deposition. Thus Na2SO4, NaCl, NaNO3 and simulated sea salt solutions were injected into the combustor of a nominal Mach 0.3 burner rig burning jet fuel at constant fuel/air ratios. The deposits formed on inert collectors, rotation in the cross flow of the combustion gases, were weighed and analyzed. Collector temperature was uniform and could be varied over a large range by internal air cooling. Deposition rates and dew point temperatures were determined. Supplemental testing included droplet size measurements of the atomized salt solutions. These tests along with thermodynamic and transport calculations were utilized in the interpretation of the deposition results.
Document ID
19840023488
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Santoro, G. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Gokoglu, S. A.
(Analex Corp. Cleveland, OH, United States)
Kohl, F. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Stearns, C. A.
(NASA Lewis Research Center)
Rosner, D. E.
(Yale Univ.)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-83751
NAS 1.15:83751
E-2237
Report Number: NASA-TM-83751
Report Number: NAS 1.15:83751
Report Number: E-2237
Meeting Information
Meeting: TMS-AIME Fall Meeting
Location: Detroit, MI
Country: United States
Start Date: September 17, 1984
End Date: September 19, 1984
Accession Number
84N31558
Funding Number(s)
PROJECT: RTOP 505-04-1A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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