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Flow Structure Comparison for Two 7-Point LDI ConfigurationsThis paper presents a comparison primarily of the 2-D velocity profiles in the non-burning system; and for the luminescent flame structure for a 7-point Lean Direct Injector (LDI). This circular LDI array consists of a center element surrounded by six outer elements spaced 60 degrees apart; the spacing between all adjacent elements is the same. Each element consists of simplex atomizer that injects at the throat of a converging-diverging venturi, and an axial swirler upstream of the venturi throat to generate swirl. The two configurations were: 1) one which consists of all 60 co-swirling axial air swirlers, and; 2) one configuration which uses a 60 swirler in the center, surrounded by counter-swirling 45 swirlers. Testing was done at 5 atm and an inlet temperature of 800F. Two air reference velocities were considered in the cold flow measurements and one common air flow condition for the burning case.The 2D velocity profiles were determined using particle image velocimetry and the flame structure was determined using high speed photography.
Document ID
20170006621
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Hicks, Yolanda R.
(NASA Glenn Research Center Cleveland, OH United States)
Tacina, Kathleen M.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
July 18, 2017
Publication Date
April 23, 2017
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN42068
Report Number: GRC-E-DAA-TN42068
Meeting Information
Meeting: U.S. National Combustion Meeting
Location: College Park, MD
Country: United States
Start Date: April 23, 2017
End Date: April 26, 2017
Sponsors: Maryland Univ.
Funding Number(s)
WBS: WBS 109492.02.03.02.30.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
velocity
combustion
lean direct injection
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