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A study of panel flutter with the exact method of ZeydelCalculating flutter boundaries and estimating stresses in infinite spanwise array of panels using exact method of Zeydel
Document ID
19710004611
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yates, J. E. (Aeronautical Research Associates of Princeton, Inc. Princeton, NJ, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1970
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
ARAP-145
NASA-CR-1721
Report Number: ARAP-145
Report Number: NASA-CR-1721
Accession Number
71N14086
Funding Number(s)
CONTRACT_GRANT: NAS8-24390
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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