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Evaluation of flow properties in a combustion- driven expansion tube operating at 7.5 km/sec.Convective and radiative heat transfer during atmospheric reentry examined, using double- diaphragm shock tube operated in expansion tube mode
Document ID
19660043538
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Givens, J. J.
Page, W. A.
Reynolds, R. M.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Facilities, Research, And Support
Accession Number
66A22828
Distribution Limits
Public
Copyright
Other
Keywords
RADIATIVE HEAT TRANSFER
ATMOSPHERIC ENTRY
SHOCK TUNNEL
CONVECTIVE HEAT TRANSFER

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