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The computation of steady nozzle flow by a time-dependent methodThe steady flow in two-dimensional and axisymmetric nozzles was computed using a time-dependent method. In this method the interior mesh points were computed using the MacCormack finite-difference scheme, while a characteristic scheme was used to calculate the boundary mesh points. No explicit artificial viscosity term was included. The fluid was assumed to be a perfect gas. This method was used to compute the flow in a 45 deg - 15 deg conical, converging-diverging nozzle, a 15 deg conical, converging nozzle, and a 10 deg conical, plug nozzle. Good agreement between the numerical solution and experimental data was found. In contrast to previous time-dependent methods, the computational times were less than one minute on a CDC 6600 computer.
Document ID
19740008900
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cline, M. C.
(Los Alamos Sci. Lab.)
Date Acquired
September 3, 2013
Publication Date
April 1, 1974
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-71918
Report Number: NASA-TM-X-71918
Accession Number
74N17013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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