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Comparison between the PISO algorithm and preconditioning methods for compressible flowTwo widely used family of algorithms, pressure-based and density-based methods, have been developed for computational fluid dynamics (CFD) problems over the years. Pressure-based methods (such as SIMPLE and PISO) use a Poisson-like equation for updating pressure instead of the continuity equation, while density-based methods use the continuity equation to update density (an equation of state is used to provide density in pressure based schemes and pressure in density based schemes). Pressure-based methods were developed originally for incompressible flows at low Reynolds numbers and were then extended to high Reynolds numbers and compressible applications. On the other hand, density based methods were originally developed for transonic flows and have been extended down to low Mach numbers through the use of preconditioning techniques. We compare these two very different approaches to solving the Navier-Stokes equations in order to gain an understanding of their similarities and differences. Specifically, we consider the PISO scheme as a representative pressure-based method and contrast it with a recently developed preconditioning scheme. We also compare the relative performance of the PISO algorithm with a Euler implicit algorithm that is employed to solve the preconditioned equations by means of a vector stability analysis.
Document ID
19920023040
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Charles L Merkle
(Pennsylvania State Univ. University Park, PA United States)
Philip E O Buelow
(Pennsylvania State Univ. University Park, PA, United States)
S Venkateswaran
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Publication Information
Publication: NASA Conference Publication 3163 Part 1
Publisher: NASA Marshall Space Flight Center
Subject Category
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1
Location: Huntsville, AL
Country: US
Start Date: April 28, 1992
End Date: April 30, 1992
Sponsors: NASA Marshall Space Flight Center
Accession Number
92N32284
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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