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Application of a supersonic kernel-function procedure to flutter analysis of thin lifting surfacesFlutter analysis for thin lifting surfaces by application of supersonic kernel function procedure
Document ID
19710001392
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Cunningham, H. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1970
Subject Category
Structural Mechanics
Report/Patent Number
L-6808
NASA-TN-D-6012
Report Number: L-6808
Report Number: NASA-TN-D-6012
Accession Number
71N10866
Funding Number(s)
CONTRACT_GRANT: 126-14-14-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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