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Experimentally Determined Effects of Varying Pitch and Control Stiffnesses on the Flutter Characteristics at Supersonic Speeds of All-movable Wing and Tail ModelsPitch and control stiffness effects on flutter characteristics of all-moveable wing and vertical and horizontal tails on fighter aircraft at supersonic speeds
Document ID
19660024794
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Hanson, P. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-MEMO-10-16-58L
Accession Number
66N34084
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER
SUPERSONIC SPEED
HORIZONTAL TAIL
VERTICAL TAIL
FIGHTER AIRCRAFT

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