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A solution procedure for three-dimensional incompressible Navier-Stokes equation and its applicationAn implicit, finite-difference procedure is presented for numerically solving viscous incompressible flows. For convenience of applying the present method to three-dimensional problems, primitive variables, namely the pressure and velocities, are used. One of the major difficulties in solving incompressible flows that use primitive variables is caused by the pressure field solution method which is used as a mapping procedure to obtain a divergence-free velocity field. The present method is designed to accelerate the pressure-field solution procedure. This is achieved by the method of pseudocompressibility in which the time derivative pressure term is introduced into the mass conservation equation. The pressure wave propagation and the spreading of the viscous effect is investigated using simple test problems. The present study clarifies physical and numerical characteristics of the pseudo-compressible approach in simulating incompressible flows. Computed results for external and internal flows are presented to verify the present procedure. The present algorithm has been shown to be very robust and accurate if the selection of the pseudo-compressibility parameter has been made according to the guidelines given.
Document ID
19840018598
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 Canoga Park, Calif., United States)
Shanks, S. P.
(Rockwell International Canoga Park, Calif., United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-85978
A-9801
NAS 1.15:85978
Report Number: NASA-TM-85978
Report Number: A-9801
Report Number: NAS 1.15:85978
Accession Number
84N26666
Funding Number(s)
PROJECT: RTOP 505-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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