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Atomization and vaporization characteristics of airblast fuel injection inside a venturi tubeThis paper describes the experimental and numerical characterization of the capillary fuel injection, atomization, dispersion, and vaporization of liquid fuel in a coflowing air stream inside a single venturi tube. The experimental techniques used are all laser-based. Phase Doppler analyzer was used to characterize the atomization and vaporization process. Planar laser-induced fluorescence visualizations give good qualitative picture of the fuel droplet and vapor distribution. Limited quantitative capabilities of the technique are also demonstrated. A modified version of the KIVA-II was used to simulate the entire spray process, including breakup and vaporization. The advantage of venturi nozzle is demonstrated in terms of better atomization, more uniform F/A distribution, and less pressure drop. Multidimensional spray calculations can be used as a design tool only if care is taken for the proper breakup model, and wall impingement process.
Document ID
19930065665
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sun, H.
(NASA Lewis Research Center Cleveland, OH, United States)
Chue, T.-H.
(NASA Lewis Research Center Cleveland, OH, United States)
Lai, M.-C.
(Wayne State Univ. Detroit, MI, United States)
Tacina, R. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 93-1766
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: SAE, AIAA, ASEE, ASME
Accession Number
93A49662
Funding Number(s)
CONTRACT_GRANT: NSF RII-88-05070
CONTRACT_GRANT: NAG3-1140
CONTRACT_GRANT: DAAL03-92-G-0168
Distribution Limits
Public
Copyright
Other

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