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SHOCK-LAYER RADIATION OF BLUNT BODIES TRAVELING AT LUNAR RETURN ENTRY VELOCITIESThermal radiation from shock layer for lunar- return reentry vehicle simulated in shock-tube- driven hypersonic wind tunnel
Document ID
19630015305
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Page, W. A.
Date Acquired
August 1, 2013
Publication Date
January 23, 1963
Subject Category
Aircraft
Report/Patent Number
IAS PAPER 63-41
Report Number: IAS PAPER 63-41
Accession Number
63A11364
Distribution Limits
Public
Copyright
Other
Keywords
THERMAL RADIATION
HYPERSONIC WIND TUNNEL
SHOCK HEATING
HEAT TRANSFER
REENTRY VEHICLE

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