NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Development of advanced Navier-Stokes solverThe objective of research was to develop and validate new computational algorithms for solving the steady and unsteady Euler and Navier-Stokes equations. The end-products are new three-dimensional Euler and Navier-Stokes codes that are faster, more reliable, more accurate, and easier to use. The three-dimensional Euler and full/thin-layer Reynolds-averaged Navier-Stokes equations for compressible/incompressible flows are solved on structured hexahedral grids. The Baldwin-Lomax algebraic turbulence model is used for closure. The space discretization is based on a cell-centered finite-volume method augmented by a variety of numerical dissipation models with optional total variation diminishing limiters. The governing equations are integrated in time by an implicit method based on lower-upper factorization and symmetric Gauss-Seidel relaxation. The algorithm is vectorized on diagonal planes of sweep using two-dimensional indices in three dimensions. Convergence rates and the robustness of the codes are enhanced by the use of an implicit full approximation storage multigrid method.
Document ID
19940032941
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yoon, Seokkwan
(MCAT Inst. San Jose, CA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Numerical Analysis
Report/Patent Number
NASA-CR-195094
MCAT-94-004
NAS 1.26:195094
Report Number: NASA-CR-195094
Report Number: MCAT-94-004
Report Number: NAS 1.26:195094
Accession Number
94N37449
Funding Number(s)
CONTRACT_GRANT: NCC2-505
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available