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A NASTRAN primer for the analysis of rotating flexible bladesThis primer provides documentation for using MSC NASTRAN in analyzing rotating flexible blades. The analysis of these blades includes geometrically nonlinear (large displacement) analysis under centrifugal loading, and frequency and mode shape (normal modes) determination. The geometrically nonlinear analysis using NASTRAN Solution sequence 64 is discussed along with the determination of frequencies and mode shapes using Solution Sequence 63. A sample problem with the complete NASTRAN input data is included. Items unique to rotating blade analyses, such as setting angle and centrifugal softening effects are emphasized.
Document ID
19870011942
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lawrence, Charles
(NASA Lewis Research Center Cleveland, OH, United States)
Aiello, Robert A.
(NASA Lewis Research Center Cleveland, OH, United States)
Ernst, Michael A.
(NASA Lewis Research Center Cleveland, OH, United States)
Mcgee, Oliver G.
(Ohio State Univ. Columbus, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1987
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-89861
NAS 1.15:89861
E-3528
Report Number: NASA-TM-89861
Report Number: NAS 1.15:89861
Report Number: E-3528
Accession Number
87N21375
Funding Number(s)
PROJECT: RTOP 505-63-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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