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Liquid sprays and flow studies in the direct-injection diesel engine under motored conditionsA two dimensional, implicit finite difference method of the control volume variety, a two equation model of turbulence, and a discrete droplet model were used to study the flow field, turbulence levels, fuel penetration, vaporization, and mixing in diesel engine environments. The model was also used to study the effects of engine speed, injection angle, spray cone angle, droplet distribution, and intake swirl angle on the flow field, spray penetration and vaporization, and turbulence in motored two-stroke diesel engines. It is shown that there are optimum conditions for injection, which depend on droplet distribution, swirl, spray cone angle, and injection angle. The optimum conditions result in good spray penetration and vaporization and in good fuel mixing. The calculation presented clearly indicates that internal combustion engine models can be used to assess, at least qualitatively, the effects of injection characteristics and engine operating conditions on the flow field and on the spray penetration and vaporization in diesel engines.
Document ID
19880009210
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Nguyen, Hung Lee
(NASA Lewis Research Center Cleveland, OH., United States)
Carpenter, Mark H.
(NASA Langley Research Center Hampton, VA., United States)
Ramos, Juan I.
(Carnegie-Mellon Univ. Pittsburgh, Pa., United States)
Schock, Harold J.
(NASA Lewis Research Center Cleveland, OH., United States)
Stegeman, James D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1988
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-100135
NAS 1.15:100135
E-3685
Report Number: NASA-TM-100135
Report Number: NAS 1.15:100135
Report Number: E-3685
Accession Number
88N18594
Funding Number(s)
PROJECT: RTOP 505-62-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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