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Composite hubs for low cost turbine enginesA detailed stress analysis is performed using NASTRAN to demonstrate theoretically the adequacy of composite hubs for low cost turbine engine applications. The results show that composite hubs are adequate for this application from the steady state stress viewpoint.
Document ID
19770063668
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Chamis, C. C. (NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: Annual Conference on Discover reinforced plastics
Location: Washington, DC
Start Date: February 8, 1977
End Date: February 11, 1977
Accession Number
77A46520
Distribution Limits
Public
Copyright
Other

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