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- W2000291829 abstract "A new design methodology is presented for cutouts in composite aircraft structure. The methodology is based on a Rayleigh-Ritz stress analysis procedure that accommodates circular and elliptical cutouts in composite panels under generalized in-plane loading conditions. Cutout padups and panel stiffener reinforcements are also included in this procedure. Panel strength calculations are performed by combining the stress analysis with a generalized version of the average stress failure criterion. Sizing procedures are given for design of padup and stiffener reinforcements in cutout panels, and an example problem is provided to illustrate typical results." @default.
- W2000291829 created "2016-06-24" @default.
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- W2000291829 date "1992-04-13" @default.
- W2000291829 modified "2023-09-27" @default.
- W2000291829 title "A Rayleigh-Ritz design methodology for cutouts in composite structures" @default.
- W2000291829 cites W1983672059 @default.
- W2000291829 doi "https://doi.org/10.2514/6.1992-2278" @default.
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