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Langley hotshot tunnel operations with helium at Mach numbers in excess of 30Temperature and pressure effects on high Mach number helium flow in hotshot wind tunnel
Document ID
19700024440
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Miller, C. G., III (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1970
Subject Category
Facilities, Research, And Support
Report/Patent Number
L-6876
NASA-TN-D-5901
Report Number: L-6876
Report Number: NASA-TN-D-5901
Accession Number
70N33751
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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