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Investigation of a 1/4-scale model of the Republic F-105 airplane in the Langley 19-foot pressure tunnel. Lateral control and directional stability and control characteristics of model equipped with drooped, supersonic-type, elliptical wing-root inlet
Document ID
19710073550
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Canoro, P. A. (NASA Langley Research Center Hampton, VA, United States)
Kelly, H. N. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
November 10, 1955
Subject Category
Unknown
Report/Patent Number
NACA-RM-SL55J10
Report Number: NACA-RM-SL55J10
Accession Number
71X72132
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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