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An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristicsAerodynamic effects of airfoil thickness on transonic flutter characteristics of swept and unswept wings
Document ID
19660024036
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Doggett, R. V., Jr. (NASA Langley Research Center Hampton, VA, United States)
Morgan, H. G. (NASA Langley Research Center Hampton, VA, United States)
Rainey, A. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-79
Report Number: NASA-TM-X-79
Accession Number
66N33326
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
UNSWEPT WING
SWEPT WING
AERODYNAMIC STABILITY
AIRFOIL THICKNESS
TRANSONIC FLUTTER

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