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Transonic flutter investigation of models of the X-15 airplane horizontal tailTransonic flutter analysis of dynamically and elastically scaled models of sweptback, tapered, all-movable horizontal tail of X-15 aircraft
Document ID
19660024039
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bland, S. R. (NASA Langley Research Center Hampton, VA, United States)
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-447
Report Number: NASA-TM-X-447
Accession Number
66N33329
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SCALE MODEL
HORIZONTAL TAIL
FLUTTER ANALYSIS
TRANSONIC FLUTTER
SWEPTBACK TAIL SURFACE
X-15 AIRCRAFT

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