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Composite Blade Structural Analyzer (COBSTRAN) demonstration manualThe input deck setup is described for a computer code, composite blade structural analyzer (COBSTRAN) which was developed for the design and analysis of composite turbofan and turboprop blades and also for composite wind turbine blades. This manual is intended for use in conjunction with the COBSTRAN user's manual. Seven demonstration problems are described with pre- and postprocessing input decks. Modeling of blades which are solid thru-the-thickness and also aircraft wing airfoils with internal spars is shown. Corresponding NASTRAN and databank input decks are also shown. Detail descriptions of each line of the pre- and post-processing decks is provided with reference to the Card Groups defined in the user's manual. A dictionary of all program variables and terms used in this manual may be found in Section 6 of the user's manual.
Document ID
19890015088
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Aiello, Robert A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1989
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-101957
E-4735
NAS 1.15:101957
Report Number: NASA-TM-101957
Report Number: E-4735
Report Number: NAS 1.15:101957
Accession Number
89N24459
Funding Number(s)
PROJECT: RTOP 505-63-1B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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