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Composite hubs for low cost gas turbine enginesA detailed stress analysis was performed using NASTRAN to demonstrate theoretically the adequacy of composite hubs for low cost turbine engine applications. Composite hubs are adequate for this application from the steady state stress view point.
Document ID
19770010123
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, C. C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-9038
NASA-TM-X-73578
Report Number: E-9038
Report Number: NASA-TM-X-73578
Meeting Information
Meeting: Annual Conf. of the Reinforced Plastics of Composites Inst.
Location: Washington, DC
Country: United States
Start Date: February 8, 1977
End Date: February 11, 1977
Sponsors: Soc. of the Plastics Ind.
Accession Number
77N17066
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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