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Focused Schlieren flow visualization studies of multiple venturi fuel injectors in a high pressure combustorMultiple venturi fuel injectors were used to obtain uniform fuel distributions, better atomization and vaporization in the premixing/prevaporizing section of a lean premixed/prevaporized flame tube combustor. A focused Schlieren system was used to investigate the fuel/air mixing effectiveness of various fuel injection configurations. The Schlieren system was focused to a plane within the flow field of a test section equipped with optical windows. The focused image plane was parallel to the axial direction of the flow and normal to the optical axis. Images from that focused plane, formed by refracted light due to density gradients within the flow field, were filmed with a high-speed movie camera at framing rates of 8,000 frames per second (fps). Three fuel injection concepts were investigated by taking high-speed movies of the mixture flows at various operating conditions. The inlet air temperature was varied from 600 F to 1000 F, and inlet pressures from 80 psia to 150 psia. Jet-A fuel was used typically at an equivalence ratio of 0.5. The intensity variations of the digitized Schlieren images were analytically correlated to spatial density gradients of the mixture flows. Qualitative measurements for degree of mixedness, intensity of mixing, and mixing completion time are shown. Various mixing performance patterns are presented with different configurations of fuel injection points and operating conditions.
Document ID
19940022070
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chun, K. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Locke, R. J.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Lee, C. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Ratvasky, W. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-8409
NASA-TM-106479
AIAA PAPER 94-0280
NAS 1.15:106479
Report Number: E-8409
Report Number: NASA-TM-106479
Report Number: AIAA PAPER 94-0280
Report Number: NAS 1.15:106479
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 1994
End Date: January 13, 1994
Sponsors: AIAA
Accession Number
94N26573
Funding Number(s)
PROJECT: RTOP 537-02-20
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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