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Numerical studies of the formation and destruction of vortices in a motored four-stroke piston-cylinder configurationA finite-difference procedure which solves the conservation equations of mass, momentum, and energy is used to investigate the effects of the compression ratio, engine speed, bore-to-stroke ratio, and air intake flow angle on the turbulent flow field within an axisymmetric piston-cylinder configuration. It is shown that in a four-stroke piston-cylinder configuration, the intake stroke is characterized by the formation of a piston vortex. The piston vortex is stretched during the intake stroke, and the head vortex has an almost constant diameter. For a 0-deg air intake flow angle, both vortices disappear by the end of the compression stroke; for an air intake flow angle of 45 deg, the flow field within the cylinder shows three elongated vortices which persist into the compression stroke and then break up and merge. It is also shown that larger bore-to-stroke ratios give rise to lower turbulent levels than smaller bore-to-stroke ratios and that the turbulent intensity is almost independent of the rpm.
Document ID
19830035531
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schock, H. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Sosoka, D. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Ramos, J. I.
(Carnegie-Mellon University Pittsburgh, PA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 83-0497
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Reno, NV
Start Date: January 10, 1983
End Date: January 13, 1983
Accession Number
83A16749
Distribution Limits
Public
Copyright
Other

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