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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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