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Low-speed investigation of effects of vertical tails on the static stability characteristics of a canard-bomber configuration having a very thin wing and a slender elliptical fuselageEffect of vertical tails on low speed static stability characteristics of canard-bomber configuration with very thin wing and slender elliptical fuselage
Document ID
19660024046
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gainer, T. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-436
Accession Number
66N33336
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOMBER AIRCRAFT
VERTICAL TAIL
STATIC STABILITY AND CONTROL
FUSELAGE
CANARD
WING TIP CONTROL

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