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Detailed fuel spray analysis techniquesDetailed fuel spray analyses are a necessary input to the analytical modeling of the complex mixing and combustion processes which occur in advanced combustor systems. It is anticipated that by controlling fuel-air reaction conditions, combustor temperatures can be better controlled, leading to improved combustion system durability. Thus, a research program is underway to demonstrate the capability to measure liquid droplet size, velocity, and number density throughout a fuel spray and to utilize this measurement technique in laboratory benchmark experiments. The research activities from two contracts and one grant are described with results to data. The experiment to characterize fuel sprays is also described. These experiments and data should be useful for application to and validation of turbulent flow modeling to improve the design systems of future advanced technology engines.
Document ID
19830026672
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mularz, E. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Bosque, M. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Humenik, F. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:83476
NASA-TM-83476
E-1792
AVRADCOM-TR-83-C-7
Report Number: NAS 1.15:83476
Report Number: NASA-TM-83476
Report Number: E-1792
Report Number: AVRADCOM-TR-83-C-7
Meeting Information
Meeting: Symp. of the Propulsion and Energetics Panel on Combust. Probl. in Turbine Eng.
Location: Cesme
Country: Turkey
Start Date: October 3, 1983
End Date: October 6, 1983
Sponsors: AGARD
Accession Number
83N34943
Funding Number(s)
PROJECT: RTOP 505-31-42
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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