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Two-dimensional analysis of two-phase reacting flow in a firing direct-injection diesel engineThe flow field, spray penetration, and combustion in two-stroke diesel engines are described. Fuel injection begins at 345 degrees after top dead center (ATDC) and n-dodecane is used as the liquid fuel. Arrhenius kinetics is used to calculate the reaction rate term in the quasi-global combustion model. When the temperature, fuel, and oxygen mass fraction are within suitable flammability limits, combustion begins spontaneously. No spark is necessary to ignite a localized high temperature region. Compression is sufficient to increase the gaseous phase temperature to a point where spontaneous chemical reactions occur. Results are described for a swirl angle of 22.5 degrees.
Document ID
19900004076
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Nguyen, H. Lee
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1989
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-102069
E-4826
NAS 1.15:102069
Report Number: NASA-TM-102069
Report Number: E-4826
Report Number: NAS 1.15:102069
Accession Number
90N13392
Funding Number(s)
PROJECT: RTOP 505-62-61
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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