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Effects of free-flight rocket-model booster-adapter configurations on the aerodynamic characteristics in pitch and sideslip of a swept-wing fighter airplane model at a Mach number of 2.01
Document ID
19710065524
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Robinson, R. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
March 25, 1955
Publication Information
Publisher: NACA
Subject Category
Unknown
Report/Patent Number
NACA-RM-L55B01
Report Number: NACA-RM-L55B01
Accession Number
71N70837
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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