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FREE-FLIGHT TESTS OF 45 DEG SWEPT WINGS OF ASPECT RATIO 3.15 AND TAPER RATIO 0.54 TO MEASURE WING DAMPING OF THE FIRST BENDING MODE AND TO INVESTIGATE THE POSSIBILITY OF FLUTTER AT TRANSONIC SPEEDSFree flight tests of 45-deg swept wings of 3.15 aspect ratio and 0.54 taper ratio to measure wing damping and possible transonic flutter
Document ID
19630003991
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Lauten, W. T., Jr. (NASA Langley Research Center Hampton, VA, United States)
Lundstrom, R. R. (NASA Langley Research Center Hampton, VA, United States)
Okelly, B. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
October 12, 1954
Subject Category
Auxiliary Systems
Report/Patent Number
NACA-RM-L54C22
Report Number: NACA-RM-L54C22
Accession Number
63N13867
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER
SWEPT WING
FREE FLIGHT
TRANSONIC FLUTTER

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