NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Vortex motion in axisymmetric piston-cylinder configurationsBy using the Beam and Warming implicit-factored method of solution of the Navier-Stokes equations, velocities were calculated inside axisymmetric piston cylinder configurations during the intake and compression strokes. Results are presented in graphical form which show the formation, growth and breakup of those vortices which form during the intake stroke by the jet issuing from the valve. It is shown that at bore-to-stroke ratio of less than unity, the vortices may breakup during the intake stroke. It is also shown that vortices which do not breakup during the intake stroke coalesce during the compression stroke.
Document ID
19830027047
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Shih, T. I. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Smith, G. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Springer, G. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-85404
NAS 1.15:85404
LOG-J13452
Report Number: NASA-TM-85404
Report Number: NAS 1.15:85404
Report Number: LOG-J13452
Accession Number
83N35318
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available