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Three-dimensional incompressible Navier-Stokes computations of internal flowsSeveral incompressible Navier-Stokes solution methods for obtaining steady and unsteady solutions are discussed. Special attention is given to internal flows which involve distinctly different features from external flows. The characterisitcs of the flow solvers employing the method of pseudocompressibility and a fractional step method are briefly described. This discussion is limited to a primitive variable formulation in generalized curvilinear coordinates. Computed results include simple test cases and internal flow in the Space Shuttle main engine hot-gas manifold.
Document ID
19880010041
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kwak, D.
(NASA Ames Research Center Moffett Field, CA., United States)
Chang, J. L. C.
(Rockwell International Corp. Canoga Park, CA., United States)
Rogers, S. E.
(Sterling Federal Systems, Inc. Palo Alto, Calif., United States)
Rosenfeld, M.
(NASA Ames Research Center Moffett Field, CA, United States)
Kwak, D.
(NASA Ames Research Center, Moffett Field CA., United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1988
Subject Category
Air Transportation And Safety
Report/Patent Number
NAS 1.15:100076
A-88111
NASA-TM-100076
Report Number: NAS 1.15:100076
Report Number: A-88111
Report Number: NASA-TM-100076
Accession Number
88N19425
Funding Number(s)
PROJECT: RTOP 505-60-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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