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SOME EFFECTS OF VARIATIONS IN DENSITY AND AERODYNAMIC PARAMETERS ON THE CALCULATED FLUTTER CHARACTERISTICS OF FINITE-SPAN SWEPT AND UNSWEPT WINGS AT SUBSONIC AND SUPERSONIC SPEEDSSubsonic and supersonic flutter calculations on swept and unswept wings to evaluate effects of variations in aerodynamic parameters and density
Document ID
19630003038
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-182
Report Number: NASA-TM-X-182
Accession Number
63N12914
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW CHARACTERISTICS
UNSWEPT WING
GAS DENSITY
AERODYNAMIC CHARACTERISTICS
SUBSONIC FLUTTER
SUPERSONIC FLUTTER

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