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EXPERIMENTAL AND CALCULATED RESULTS OF A FLUTTER INVESTIGATION OF SOME VERY LOW ASPECT-RATIO FLAT-PLATE SURFACES AT MACH NUMBERS FROM 0.62 TO 3.00Flutter investigation of very low aspect-ratio flat-plate surfaces at subsonic and supersonic speed
Document ID
19630003076
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hanson, P. W. (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
August 1, 1959
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-53
Report Number: NASA-TM-X-53
Accession Number
63N12952
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ALUMINUM ALLOY
PLANFORM
FLAT PLATE
SUBSONIC FLUTTER
LOW ASPECT RATIO WING
SUPERSONIC FLUTTER

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