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Dynamic analysis of pretwisted elastically-coupled rotor bladesThis paper addresses the accuracy of using a one-dimensional analysis to predict frequencies of elastically-coupled highly-twisted rotor blades. 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
19930037128
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nixon, Mark W.
(NASA Langley Research Center Hampton, VA, United States)
Hinnant, Howard E.
(U.S. Army, Aerostructures Directorate; NASA, Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
November 1, 1992
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: ASME, Winter Annual Meeting
Location: Anaheim, CA
Country: United States
Start Date: November 8, 1992
End Date: November 13, 1992
Sponsors: ASME
Accession Number
93A21125
Distribution Limits
Public
Copyright
Other

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