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Transonic flutter investigation of models of proposed horizontal tails for the X-15 airplaneTransonic flutter analysis of dynamically and elastically scaled models of all-movable horizontal tail of X-15 aircraft
Document ID
19660024038
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Young, L. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-442
Report Number: NASA-TM-X-442
Accession Number
66N33328
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRANSONIC FLUTTER
FLUTTER ANALYSIS
HORIZONTAL TAIL
SCALE MODEL
X-15 AIRCRAFT

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