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Study of equilibrium air total radiation.Equilibrium air total radiation mechanism, vacuum UV radiation and relation to hypervelocity entry studied, using shock tube blunt model test flow
Document ID
19670041840
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Gruszczynski, J. S.
Warren, W. R., Jr.
Date Acquired
August 3, 2013
Publication Date
March 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 66-103
Report Number: AIAA PAPER 66-103
Accession Number
67A20569
Funding Number(s)
CONTRACT_GRANT: NASW-1303
CONTRACT_GRANT: NASW-939
Distribution Limits
Public
Copyright
Other
Keywords
VACUUM ULTRAVIOLET
SHOCK TUNNEL
EQUILIBRIUM FLOW
HIGH TEMPERATURE AIR
HYPERVELOCITY PROJECTILE
ATMOSPHERIC RADIATION

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