27th Aerospace Sciences Meeting 1989
DOI: 10.2514/6.1989-122
|View full text |Cite
|
Sign up to set email alerts
|

Unified formulation for incompressible flows

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
28
0

Year Published

1991
1991
2009
2009

Publication Types

Select...
6
3

Relationship

2
7

Authors

Journals

citations
Cited by 57 publications
(28 citation statements)
references
References 7 publications
0
28
0
Order By: Relevance
“…(11) and (12) contain the variable (and therefore ), the steady-state solution has a dependency on , where larger values correspond to increased dissipation. 32 Numerical experiments have indicated that this influence is small for values of below approximately 100. Also, since large values of correspond to large values of , if is chosen to be very large, there is a wide disparity in the magnitudes of the eigenvalues.…”
Section: Finite-volume Schemementioning
confidence: 99%
“…(11) and (12) contain the variable (and therefore ), the steady-state solution has a dependency on , where larger values correspond to increased dissipation. 32 Numerical experiments have indicated that this influence is small for values of below approximately 100. Also, since large values of correspond to large values of , if is chosen to be very large, there is a wide disparity in the magnitudes of the eigenvalues.…”
Section: Finite-volume Schemementioning
confidence: 99%
“…Recently, a new time accurate, primitive variable approach has become more and more popular for solving incompressible flows [19], [20], [21]. This method is known as the artificial compressibility method^ and was initially proposed by Chorin [22] for steady flow cal culations.…”
Section: Two-dimensional Compressible Flowsmentioning
confidence: 99%
“…More recently, investigators [19], [20], [21] have suggested that the procedure can be made accurate with respect to time by considering the time-like variable appearing in the fictitious time term added to the continuity equation to be a pseudotime. For each physical time step, the pseudotime is advanced several increments in an iterative fashion.…”
Section: Three-dimensional Incompressible Liquid Sloshing Flowsmentioning
confidence: 99%
“…Pan and Chakravarthy [26] have shown that for the form of the incompressible flow equations used in this study the Roe average turns out to be just the simple arithmetic average. Equation (5.3.1) can be used to find the flux at cell center i+l in terms of the flux at i.…”
Section: Governing Equations Of a Thermohaline Ocean With Respect To mentioning
confidence: 99%