NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A numerical study of three-dimensional vortex breakdownA numerical simulation of bubble-type vortex breakdown using a unique discrete form of the full 3-D, unsteady incompressible Navier-Stokes equations was performed. The Navier-Stokes equations were written in a vorticity-velocity form and the physical problem was not restricted to axisymmetric flow. The problem was parametized on a Rossby- Reynolds-number basis. Utilization of this parameter duo was shown to dictate the form of the free-field boundary condition specification and allowed control of axial breakdown location within the computational domain. The structure of the breakdown bubble was studied through time evolution plots of planar projected velocity vectors as well as through plots of particle traces and vortex lines. These results compared favorably with previous experimental studies. In addition, profiles of all three velocity components are presented at various axial stations and a Fourier analysis was performed to identify the dominant circumferential modes. The dynamics of the breakdown process were studied through plots of axial variation of rate of change of integrated total energy and rate of change of integrated enstrophy, as well as through contour plots of velocity, vorticity and pressure.
Document ID
19870016563
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Spall, Robert E.
(Old Dominion Univ. Norfolk, VA, United States)
Ash, Robert L.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-181068
NAS 1.26:181068
Report Number: NASA-CR-181068
Report Number: NAS 1.26:181068
Accession Number
87N25996
Funding Number(s)
CONTRACT_GRANT: NAG1-530
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available