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EFFECTS OF WING VERTICAL LOCATION ON THE STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A CANARD AIRPLANE CONFIGURATION WITH A TRAPEZOIDAL ASPECT-RATIO-3 WINGEffects of wing vertical location on stability and control of canard aircraft at supersonic speeds
Document ID
19630002675
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Foster, G. V. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-44
Report Number: NASA-TM-X-44
Accession Number
63N12551
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRCRAFT CONTROL
SUPERSONIC SPEED
WING
AERODYNAMICS
AIRCRAFT
STABILITY AND CONTROL
BODY-WING COMBINATION

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