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Measurement of Ultraviolet Radiative Heating Augmentation in HIEST Reflected Shock TunnelRadiance measurements in air at enthalpies from 8-20 MJkg have been made over a 250mm diameter flat-faced test article in Japan Aerospace Exploration Agency's HIgh-Enthalpy Shock Tunnel (HIEST). Measurements were made in the ultraviolet region (200-400 nm wavelength) in an attempt to resolve the long-standing discrepancy between theoryand measurements of heat flux over a blunt body; this discrepancy is often attributed toradiation. The spectra obtained indicate the presence of atomic iron vapor in the flowfield.At the highest enthalpies, the radiance is at the blackbody limit. An attempt to model theradiance is made by taking a nominal CFD flowfield without any contamination productsand processing it through a line-by-line radiation simulation tool. Iron vapor is introducedinto the shocked gas ahead of the model and radiation computations are repeated; the molefraction of iron vapor is adjusted to match the data. For the higher enthalpy conditions, theradiance was strongly absorbed and it was necessary to adjust the temperature and NOdensity in the freestream to match the signal below 300 nm. Once the observed spectrawere satisfactorily matched, the radiance to the stagnation point was then computed. It isshown that the impurity radiation is sufficiently large to explain the discrepancy.



Document ID
20190027602
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Cruden, Brett A.
(Engineering Research and Consulting (ERC), Inc. Moffett Field, CA, United States)
Brandis, Aaron M.
(Engineering Research and Consulting (ERC), Inc. Moffett Field, CA, United States)
Olejniczak, Joseph
(NASA Ames Research Center Moffett Field, CA, United States)
Grinstead, Jay
(NASA Ames Research Center Moffett Field, CA, United States)
Kirk, Lindsay
(NASA Johnson Space Center Houston, TX, United States)
Tanno, Hideyuki
(Japan Aerospace Exploration Agency Chofu, Japan)
Komuro, Tomoyuki
(Japan Aerospace Exploration Agency Chofu, Japan)
Date Acquired
July 23, 2019
Publication Date
May 19, 2015
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN23557
Report Number: ARC-E-DAA-TN23557
Meeting Information
Meeting: AIAA Thermophysics Conference
Location: Dallas, TX
Country: United States
Start Date: June 22, 2014
End Date: June 26, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA10DE12C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Shock Tunnel
Spectroscopy
CFD
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