A design and structural analysis of a CH-54B main rotor hub fabricated from composite materials was made to assess the flightworthiness of a hub consisting basically of tension straps fabricated from graphite epoxy and fiberglass. The concept is feasible but not competitive with the production titanium hub from a weight standpoint. (Author)
Design Analysis of CH-54B Main Rotor Hub Fabricated from Composite Materials
1973
238 pages
Report
Keine Angabe
Englisch
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