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- W2077271520 abstract "Aluminum-lithium (Al-Li) alloys represent an area of considerable interest to the aircraft industry because of the potential for high structural efficiencies compared to conventional alloy products. The reported work addresses the identification and characterization of a candidate Al-Li alloy that demonstrates promise for use in 7075 aluminum structural applications. Heat treatment studies were conducted initially to select a suitable combination of strength, ductility, and toughness. Mechanical property evaluations comprising static and cyclic testing were subsequently performed on extruded bar materials, and compared to baseline 7075 aluminum extrusions. The structural behavior was established by compression testing of stiffened panels, typical of those used in airframe construction. Experimental findings and predictions are discussed in terms of the properties of materials. A structural weight savings of between 8 and 13% was shown for Al-Li alloy materials in compression critical components." @default.
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- W2077271520 date "1988-11-01" @default.
- W2077271520 modified "2023-09-23" @default.
- W2077271520 title "Evaluation of aluminum-lithium alloys in compression-stiffened aircraft structures" @default.
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- W2077271520 doi "https://doi.org/10.2514/3.45695" @default.
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