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Large displacements and stability analysis of nonlinear propeller structuresThe use of linear rigid formats in COSMIC NASTRAN without DMAP procedures for the analysis of nonlinear propeller structures is described. Approaches for updating geometry and applying follower forces for incremental loading are demonstrated. Comparisons are made with COSMIC NASTRAN rigid formats and other independent finite element programs. Specifically, the comparisons include results from the four approaches for updating the geometry using RIGID FORMAT 1, RIGID FORMATS 4 and 13, MARC and MSC/NASTRAN. It is shown that 'user friendly' updating approaches (without DMAPS) can be used to predict the large displacements and instability of these nonlinear structures. These user friendly approaches can be easily implemented by the user and predict conservative results.
Document ID
19820023831
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Aiello, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:82850
NASA-TM-82850
Report Number: NAS 1.15:82850
Report Number: NASA-TM-82850
Accession Number
82N31707
Funding Number(s)
PROJECT: RTOP 505-33-62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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