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Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected wing tips for longitudinal and directional stability
Document ID
19650018341
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bright, L. G. (NASA Ames Research Center Moffett Field, CA, United States)
Peterson, V. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-392
Report Number: NASA-TM-X-392
Accession Number
65N27942
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
DIRECTIONAL STABILITY
CANARD
LONGITUDINAL STABILITY
WING TIP CONTROL

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