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Dynamic analysis of pretwisted elastically-coupled rotor bladesThe accuracy of using a one-dimensional analysis to predict frequencies of elastically-coupled highly-twisted rotor blades is addressed. Degrees of freedom associated with shear deformation are statically condensed from the formulation, so the analysis uses only those degrees of freedom associated with classical beam theory. The effects of cross section deformation (warping) are considered, and are shown to become significant for some types of elastic coupling. Improved results are demonstrated for highly-coupled blade structures through account of warping in a local cross section analysis, without explicit inclusion of these effects in the beam analysis. A convergence study is also provided which investigates the potential for improving efficiency of elastically-coupled beam analysis through implementation of a p-version beam finite element.
Document ID
19940020366
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nixon, Mark W.
(NASA Langley Research Center Hampton, VA, United States)
Hinnant, Howard E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-109070
NAS 1.15:109070
Report Number: NASA-TM-109070
Report Number: NAS 1.15:109070
Meeting Information
Meeting: 1992 ASME Winter Annual Meeting
Location: Anaheim, CA
Country: United States
Start Date: November 8, 1992
End Date: November 13, 1992
Accession Number
94N24839
Funding Number(s)
PROJECT: RTOP 505-63-50-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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