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User's guide to the NOZL3D and NOZLIC computer programsComplete FORTRAN listings and running instructions are given for a set of computer programs that perform an implicit numerical solution to the unsteady Navier-Stokes equations to predict the flow characteristics and performance of nonaxisymmetric nozzles. The set includes the NOZL3D program, which performs the flow computations; the NOZLIC program, which sets up the flow field initial conditions for general nozzle configurations, and also generates the computational grid for simple two dimensional and axisymmetric configurations; and the RGRIDD program, which generates the computational grid for complicated three dimensional configurations. The programs are designed specifically for the NASA-Langley CYBER 175 computer, and employ auxiliary disk files for primary data storage. Input instructions and computed results are given for four test cases that include two dimensional, three dimensional, and axisymmetric configurations.
Document ID
19840021081
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Thomas, P. D.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:159173
LMSC-D636857
NASA-CR-159173
Report Number: NAS 1.26:159173
Report Number: LMSC-D636857
Report Number: NASA-CR-159173
Accession Number
84N29150
Funding Number(s)
CONTRACT_GRANT: NAS1-15084
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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