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Effects of boundary-layer suction and spoilers on transonic flutter derivatives for a midspan control surface on an upswept wingBoundary layer suction and spoiler effects on transonic flutter derivatives for midspan control surface on unswept wing
Document ID
19660024025
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dannenberg, R. E. (NASA Ames Research Center Moffett Field, CA, United States)
Gambucci, B. J. (NASA Ames Research Center Moffett Field, CA, United States)
Sorenson, R. M. (NASA Ames Research Center Moffett Field, CA, United States)
Wyss, J. A. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-160
Report Number: NASA-TM-X-160
Accession Number
66N33315
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOUNDARY LAYER
TRANSONIC FLUTTER
SUCTION
UNSWEPT WING
SPOILER
CONTROL SURFACE

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