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Experimental study of radiation cooling effects in a hypervelocity shock layer.Radiative energy emission by blunt vehicle shock layer under severe entry conditions, discussing flow properties and radiative transfer coupling
Document ID
19690056427
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gruszczynski, J. S.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 69-719
Report Number: AIAA PAPER 69-719
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, FLUID AND PLASMA DYNAMICS CONFERENCE
Location: SAN FRANCISCO, CALIF.
Start Date: June 16, 1969
End Date: June 18, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A34416
Funding Number(s)
CONTRACT_GRANT: NASW-1587
Distribution Limits
Public
Copyright
Other

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