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- W379394496 abstract "The overall procedures for developing composite material static and fatigue design allowables are presented. The allowables are established at the material lamina level accounting for a range of environmental conditions. Design values are derived from an interpolation method, which was confirmed by screening tests. Static test results are presented as a percentage of mean room temperature dry strength and show that the environmental effects are more pronounced for the matrix modes than for the fiber modes of fracture. Kevlar/epoxy is more sensitive to the environmental design conditions than graphite/epoxy. Fatigue test results are presented in a constant-life diagram as a percentage of room temperature wet static tensile strength. The constant-life fatigue diagram shows that the tension-compression and compression-compression range may be the governing aspect for fatigue design. Statistical evaluations are made and indicate normal distribution, and relatively small sample sizes are sufficient to establish reliable design allowables." @default.
- W379394496 created "2016-06-24" @default.
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- W379394496 date "2009-03-17" @default.
- W379394496 modified "2023-09-26" @default.
- W379394496 title "Developing Design Allowables for Composite Helicopter Structures" @default.
- W379394496 doi "https://doi.org/10.1520/stp29310s" @default.
- W379394496 hasPublicationYear "2009" @default.
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