NASA Technical Reports Server (NTRS) 19980018039: Numerical Procedu... | |
by NASA Technical Reports Server (NTRS) | |
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Two primitive variable, pressure based, flux-split, | |
RNS/NS solution procedures for viscous flows are | |
presented. Both methods are uniformly valid across the | |
full Mach number range, Le., from the incompressible | |
limit to high supersonic speeds. The first method is an | |
'optimized' version of a previously developed global | |
pressure relaxation RNS procedure. Considerable reduction | |
in the number of relatively expensive matrix inversion, | |
and thereby in the computational time, has been achieved | |
with this procedure. CPU times are reduced by a factor of | |
15 for predominantly elliptic flows (incompressible and | |
low subsonic). The second method is a time-marching, | |
'linearized' convection RNS/NS procedure. The key to the | |
efficiency of this procedure is the reduction to a single | |
LU inversion at the inflow cross-plane. The remainder of | |
the algorithm simply requires back-substitution with this | |
LU and the corresponding residual vector at any cross- | |
plane location. This method is not time-consistent, but | |
has a convective-type CFL stability limitation. Both | |
formulations are robust and provide accurate solutions | |
for a variety of internal viscous flows to be provided | |
herein. | |
Date Published: 2016-10-15 02:42:42 | |
Identifier: NASA_NTRS_Archive_19980018039 | |
Item Size: 33037553 | |
Language: english | |
Media Type: texts | |
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