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Free-flight Investigation at Transonic Speeds of Drag Coefficients of a Boattail Body of Revolution with a Simulated Turbojet Exhaust Issuing at the Base from Conical Short-length Ejectors
Document ID
19930089568
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Falanga, Ralph A
Leiss, Abraham
Date Acquired
August 16, 2013
Publication Date
December 13, 1956
Report/Patent Number
NACA-RM-L56H23
Report Number: NACA-RM-L56H23
Accession Number
93R18858
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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