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Study of non-equilibrium transport phenomenaNonequilibrium phenomena due to real gas effects are very important features of low density hypersonic flows. The shock shape and emitted nonequilibrium radiation are identified as the bulk flow behavior parameters which are very sensitive to the nonequilibrium phenomena. These parameters can be measured in shock tubes, shock tunnels, and ballistic ranges and used to test the accuracy of computational fluid dynamic (CFD) codes. Since the CDF codes, by necessity, are based on multi-temperature models, it is also desirable to measure various temperatures, most importantly, the vibrational temperature. The CFD codes would require high temperature rate constants, which are not available at present. Experiments conducted at the NASA Electric Arc-driven Shock Tube (EAST) facility reveal that radiation from steel contaminants overwhelm the radiation from the test gas. For the measurement of radiation and the chemical parameters, further investigation and then appropriate modifications of the EAST facility are required.
Document ID
19870011532
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sharma, Surendra P.
(Eloret Corp. Palo Alto, CA, United States)
Date Acquired
September 5, 2013
Publication Date
May 12, 1987
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-180441
NAS 1.26:180441
Report Number: NASA-CR-180441
Report Number: NAS 1.26:180441
Accession Number
87N20965
Funding Number(s)
CONTRACT_GRANT: NCC2-418
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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