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Acoustic fatigue life prediction for nonlinear structures with multiple resonant modesThis report documents an effort to develop practical and accurate methods for estimating the fatigue lives of complex aerospace structures subjected to intense random excitations. The emphasis of the current program is to construct analytical schemes for performing fatigue life estimates for structures that exhibit nonlinear vibration behavior and that have numerous resonant modes contributing to the response.
Document ID
19920021744
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Miles, R. N.
(State Univ. of New York Binghamton, NY, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-190471
NAS 1.26:190471
Report Number: NASA-CR-190471
Report Number: NAS 1.26:190471
Accession Number
92N30988
Funding Number(s)
CONTRACT_GRANT: NAG1-978
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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