NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
A boundary element method for unsteady viscous flowsA potential vorticity method for the analysis of unsteady viscous incompressible flow past arbitrarily shaped objects is discussed which is based on the Helmholtz decomposition. It is found that the correct boundary condition to be imposed is on the normal component of the velocity for the cases of both inviscid and viscous flows. The no-slip condition is shown to be automatically satisfied for viscous flows. Numerical solutions for two-dimensional flow problems are given for attached flows in addition to those involving separation. The vorticity is confined, at least for the case of symmetric flows, to a small region in the immediate vicinity of the body, making possible the minimization of the number of node points in the field, and hence the computational time, without loss of accuracy.
Document ID
19880026043
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bharadvaj, B. K.
(Boston Univ. Boston, MA, United States)
Morino, L.
(Boston Univ. Boston, MA, United States)
Del Marco, S.
(Boston University MA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Meeting Information
Meeting: Betech 86
Location: Cambridge, MA
Country: United States
Start Date: June 17, 1986
End Date: June 19, 1986
Accession Number
88A13270
Funding Number(s)
CONTRACT_GRANT: NAG1-564
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available