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On solving the compressible Navier-Stokes equations for unsteady flows at very low Mach numbersThe properties of a preconditioned, coupled, strongly implicit finite difference scheme for solving the compressible Navier-Stokes equations in primitive variables are investigated for two unsteady flows at low speeds, namely the impulsively started driven cavity and the startup of pipe flow. For the shear-driven cavity flow, the computational effort was observed to be nearly independent of Mach number, especially at the low end of the range considered. This Mach number independence was also observed for steady pipe flow calculations; however, rather different conclusions were drawn for the unsteady calculations. In the pressure-driven pipe startup problem, the compressibility of the fluid began to significantly influence the physics of the flow development at quite low Mach numbers. The present scheme was observed to produce the expected characteristics of completely incompressible flow when the Mach number was set at very low values. Good agreement with incompressible results available in the literature was observed.
Document ID
19940012655
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pletcher, R. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Chen, K.-H.
(Ohio Aerospace Inst. Brook Park., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICOMP-93-42
NASA-TM-106380
E-8193
AIAA PAPER 93-3368
NAS 1.15:106380
Report Number: ICOMP-93-42
Report Number: NASA-TM-106380
Report Number: E-8193
Report Number: AIAA PAPER 93-3368
Report Number: NAS 1.15:106380
Meeting Information
Meeting: Fluid Dynamics Conference
Location: orlando, FL
Country: United States
Start Date: July 6, 1993
End Date: July 9, 1993
Sponsors: AIAA
Accession Number
94N17128
Funding Number(s)
PROJECT: RTOP 505-90-5K
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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