NASA NTRS · 19770063668
Composite hubs for low cost turbine engines
Abstract
A 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.
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Chamis, C. C.. 1977-01-01. Composite hubs for low cost turbine engines. https://ntrs.nasa.gov/citations/19770063668
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