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The NATA code; theory and analysis. Volume 2: User's manualThe NATA code is a computer program for calculating quasi-one-dimensional gas flow in axisymmetric nozzles and rectangular channels, primarily to describe conditions in electric archeated wind tunnels. The program provides solutions based on frozen chemistry, chemical equilibrium, and nonequilibrium flow with finite reaction rates. The shear and heat flux on the nozzle wall are calculated and boundary layer displacement effects on the inviscid flow are taken into account. The program contains compiled-in thermochemical, chemical kinetic and transport cross section data for high-temperature air, CO2-N2-Ar mixtures, helium, and argon. It calculates stagnation conditions on axisymmetric or two-dimensional models and conditions on the flat surface of a blunt wedge. Included in the report are: definitions of the inputs and outputs; precoded data on gas models, reactions, thermodynamic and transport properties of species, and nozzle geometries; explanations of diagnostic outputs and code abort conditions; test problems; and a user's manual for an auxiliary program (NOZFIT) used to set up analytical curvefits to nozzle profiles.
Document ID
19760014365
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bade, W. L.
(Avco Systems Div. Wilmington, MA, United States)
Yos, J. M.
(Avco Systems Div. Wilmington, MA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AVSD-0068-75-CR-VOL-2
NASA-CR-141743
Report Number: AVSD-0068-75-CR-VOL-2
Report Number: NASA-CR-141743
Accession Number
76N21453
Funding Number(s)
CONTRACT_GRANT: NAS9-9744
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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