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Finite element analysis of flexible, rotating bladesA reference guide that can be used when using the finite element method to approximate the static and dynamic behavior of flexible, rotating blades is given. Important parameters such as twist, sweep, camber, co-planar shell elements, centrifugal loads, and inertia properties are studied. Comparisons are made between NASTRAN elements through published benchmark tests. The main purpose is to summarize blade modeling strategies and to document capabilities and limitations (for flexible, rotating blades) of various NASTRAN elements.
Document ID
19870016952
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mcgee, Oliver G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1987
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:89906
NASA-TM-89906
E-3674
Report Number: NAS 1.15:89906
Report Number: NASA-TM-89906
Report Number: E-3674
Accession Number
87N26385
Funding Number(s)
PROJECT: RTOP 535-03-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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