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Investigation of spray dispersion and particulate formation in diesel fuel flamesAn experimental study of electrostatical atomized and dispersed diesel fuel jets was conducted at various back pressures to 40 atm. A new electrostatic injection technique was utilized to generate continuous, stable fuel sprays at charge densities of 1.5 to 2.0 C/m3 of fluid at one atm, and about 1.0 C/m3 at 40 atm. Flowrates were varied from 0.5 to 2.5 ml/s and electric potentials to -18 kV. Visual observations showed that significant enhanced dispersion of charged fuel jets occurred at high back pressures compared to aerodynamic breakup and dispersion. The average drop size was about the same as the spray triode orifice diameter, and was between the Kelly theory and the Rayleigh limit. The ignition tests, done only at one atm, indicated stable combustion of the electrostatically dispersed fuel jets.
Document ID
19890010844
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Back, L. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bankston, C. P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kwack, E. Y.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bellan, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Harstad, K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
August 15, 1988
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
AD-A201079
NASA-CR-184820
NAS 1.26:184820
JPL-D-5704
ARO-21092.6-EG
Report Number: AD-A201079
Report Number: NASA-CR-184820
Report Number: NAS 1.26:184820
Report Number: JPL-D-5704
Report Number: ARO-21092.6-EG
Accession Number
89N20215
Funding Number(s)
CONTRACT_GRANT: MIPR-109-86
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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