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Flight investigation at Mach numbers from 0.8 to 1.5 to determine the effects of nose bluntness on the total drag of two fin-stabilized bodies of revolution
Document ID
19930086389
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hart, Roger G
Date Acquired
August 29, 2013
Publication Date
October 16, 1950
Report/Patent Number
NACA-RM-L50I08a
Report Number: NACA-RM-L50I08a
Accession Number
93R15679
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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