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A Free-flight Investigation of the Effects of a Sonic Jet on the Total-drag and Base-pressure Coefficients of a Boattail Body of Revolution from Mach Number 0.83 to 1.70
Document ID
19930089157
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Falanga, Ralph A
Date Acquired
August 16, 2013
Publication Date
March 8, 1956
Report/Patent Number
NACA-RM-L55L21
Report Number: NACA-RM-L55L21
Accession Number
93R18447
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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