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USE OF EXPERIMENTAL STEADY-FLOW AERODYNAMIC PARAMETERS IN THE CALCULATION OF FLUTTER CHARACTERISTICS FOR FINITE-SPAN SWEPT ON UNSWEPT WINGS AT SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDSAerodynamic load and flutter on swept and unswept wings at various speeds
Document ID
19630004021
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Yates, E. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1960
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TM-X-183
Report Number: NASA-TM-X-183
Accession Number
63N13897
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC LOAD
SWEPT WING
UNSWEPT WING
FLUTTER

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