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Investigation of an all-movable control surface at a mach number of 6.86 for possible flutterMovable tail surface for aircraft control without flutter using X-15 scale model at hypersonic speed
Document ID
19650023668
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Armstrong, W. O. (NASA Langley Research Center Hampton, VA, United States)
Lauten, W. T., Jr. (NASA Langley Research Center Hampton, VA, United States)
Levey, G. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 8, 1958
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L58B27
Report Number: NACA-RM-L58B27
Accession Number
65N33269
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
X-15 AIRCRAFT
SCALE MODEL
TAIL SURFACE
AIRCRAFT CONTROL
AERODYNAMIC FORCE
MODE SHAPE

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