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Validation of Multitemperature Nozzle Flow CodeA computer code nozzle in n-temperatures (NOZNT), which calculates one-dimensional flows of partially dissociated and ionized air in an expanding nozzle, is tested against three existing sets of experimental data taken in arcjet wind tunnels. The code accounts for the differences among various temperatures, i.e., translational-rotational temperature, vibrational temperatures of individual molecular species, and electron-electronic temperature, and the effects of impurities. The experimental data considered are (1) the spectroscopic emission data; (2) electron beam data on vibrational temperature; and (3) mass-spectrometric species concentration data. It is shown that the impurities are inconsequential for the arcjet flows, and the NOZNT code is validated by numerically reproducing the experimental data.
Document ID
19970011363
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Park, Chul
(National Aeronautics and Space Administration. Ames Research Center Moffett Field, CA United States)
Lee, Seung -Ho.
(Eloret Corp. Palo Alto, CA United States)
Date Acquired
August 17, 2013
Publication Date
July 7, 1994
Publication Information
Publication: Journal of Thermophysics and Heat Transfer
Publisher: American Inst. of Aeronautics and Astronautics
Volume: 9
Issue: 1
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:111818
AIAA Paper 23-2862
NASA-TM-111818
Meeting Information
Meeting: AIAA Thermophysics Conference
Location: Orlando, FL
Country: United States
Start Date: July 6, 1993
End Date: July 9, 1993
Accession Number
97N70793
Funding Number(s)
CONTRACT_GRANT: NCC2-420
Distribution Limits
Public
Copyright
Public Use Permitted.
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