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Computational experience with a three-dimensional rotary engine combustion modelA new computer code was developed to analyze the chemically reactive flow and spray combustion processes occurring inside a stratified-charge rotary engine. Mathematical and numerical details of the new code were recently described by the present authors. The results are presented of limited, initial computational trials as a first step in a long-term assessment/validation process. The engine configuration studied was chosen to approximate existing rotary engine flow visualization and hot firing test rigs. Typical results include: (1) pressure and temperature histories, (2) torque generated by the nonuniform pressure distribution within the chamber, (3) energy release rates, and (4) various flow-related phenomena. These are discussed and compared with other predictions reported in the literature. The adequacy or need for improvement in the spray/combustion models and the need for incorporating an appropriate turbulence model are also discussed.
Document ID
19900016959
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Raju, M. S.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Willis, E. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-5249
NASA-TM-103104
NAS 1.15:103104
Report Number: E-5249
Report Number: NASA-TM-103104
Report Number: NAS 1.15:103104
Meeting Information
Meeting: Joint Symposium on General Aviation Systems
Location: Ocean City, NJ
Country: United States
Start Date: April 11, 1990
End Date: April 12, 1990
Sponsors: FAA, AIAA
Accession Number
90N26275
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
PROJECT: RTOP 505-62-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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