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Joint research effort on vibrations of twisted plates, phase 1: Final resultsThe complete theoretical and experimental results of the first phase of a joint government/industry/university research study on the vibration characteristics of twisted cantilever plates are given. The study is conducted to generate an experimental data base and to compare many different theoretical methods with each other and with the experimental results. Plates with aspect ratios, thickness ratios, and twist angles representative of current gas turbine engine blading are investigated. The theoretical results are generated by numerous finite element, shell, and beam analysis methods. The experimental results are obtained by precision matching a set of twisted plates and testing them at two laboratories. The second and final phase of the study will concern the effects of rotation.
Document ID
19860001112
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Reference Publication (RP)
Authors
Kielb, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Leissa, A. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Macbain, J. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Carney, K. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1985
Subject Category
Structural Mechanics
Report/Patent Number
E-2576
NASA-RP-1150
NAS 1.61:1150
Report Number: E-2576
Report Number: NASA-RP-1150
Report Number: NAS 1.61:1150
Accession Number
86N10579
Funding Number(s)
PROJECT: RTOP 505-33-78
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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