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A 6-INCH SUBSONIC HIGH-TEMPERATURE ARC TUNNEL FOR STRUCTURES AND MATERIAL TESTSSubsonic high temperature arc heated wind tunnel tests for structural materials
Document ID
19630005469
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Brown, R. D. (NASA Langley Research Center Hampton, VA, United States)
Levin, L. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1963
Subject Category
Electronics
Report/Patent Number
NASA-TN-D-1621
Report Number: NASA-TN-D-1621
Accession Number
63N15345
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HIGH TEMPERATURE
STRUCTURAL MATERIAL
ARC HEATING
SUBSONIC WIND TUNNEL

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