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HEAT TRANSFER TO BLUNT AXIALLY SYMMETRIC BODIESComparison of heat transfer rates to blunt bodies of revolution & evaluation of effects of body-nose geometry on heat transfer rates
Document ID
19630002685
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Reller, J. O., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1960
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-391
Report Number: NASA-TM-X-391
Accession Number
63N12561
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BLUNT BODY
NOSE
BODY OF REVOLUTION
LAMINAR BOUNDARY LAYER
AERODYNAMIC HEAT TRANSFER
AERODYNAMICS

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