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Investigation of aerodynamic characteristics of an airplane configuration having tail surfaces outboard of the wing tips at Mach numbers of 2.30, 2.97, and 3.51Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at supersonic speeds - wind tunnel stability test
Document ID
19660024041
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Church, J. D. (NASA Langley Research Center Hampton, VA, United States)
Hayes, W. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Sleeman, W. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 23, 1958
Subject Category
Aircraft
Report/Patent Number
NACA-RM-L58C25
Accession Number
66N33331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
AIRCRAFT CONFIGURATION
WING TIP
TAIL SURFACE
WIND TUNNEL STABILITY TEST
SUPERSONIC SPEED

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