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- W3150282757 abstract "SUMMARY OF RESULTS Structural performance has been evaluated experimentally and analytically on a boron-epoxy-reinforced titanium drag strut con- taining bonded scarf joints. Weight savings of 30 percent over existing all-metal components have been achieved in a fabricated part that was designed with conservative margins of safety. The results of this investigation are summarized as follows: 1. The drag strut was exposed to two lifetimes of fatigue load- ing and loaded in tension and compression to the respective design ultimate loads without the occurrence of any detectable damage. 2. The analytical study indicated that the peak shear stresses in the bonded joints were sufficiently low to preclude drag-strut failure by disbonding of the joints due to fatigue loading. 3. The analytical study indicated that the peak shear stresses in the bonded joints were sufficiently low to preclude drag-strut failure by disbonding of the joints due to static loading. 4. The analytical study indicated that" @default.
- W3150282757 created "2021-04-13" @default.
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- W3150282757 date "1976-01-01" @default.
- W3150282757 modified "2023-09-27" @default.
- W3150282757 title "BORON-EPOXY-REINFORCED TITANIUM AIRCRAFT LANDING-GEAR DRAG STRUT" @default.
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- W3150282757 hasPublicationYear "1976" @default.
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