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Showing 1 to 3 of 3 for “"fuselage frame"”.
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Impact Response and Failure of a Textile Composite Fuselage Frame
… are performed on two circular circumferential frame segments using a drop tower apparatus. These frames have a nominal radius of 120 inches, a forty-eight - degree included angle, a thin-walled cross section in the shape of the letter J, and are typical of the transverse fuselage frames found …
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Development of a Progressive Failure Finite Element Analysis For a Braided Composite Fuselage Frame
… are then implemented in a FEA of a circular fuselage frame of the same cross section and material for which test data was available. This circular frame test article had a nominal radius of 120 inches, a forty-eight degree included angle, and was subjected to a quasi-static, radially inward …
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Optimal design of composite fuselage frames for crashworthiness
… to address the problem of designing composite fuselage frames for crashworthiness. A key feature of any optimization strategy for increasing structural crashworthiness is a progressive failure analysis. Currently, the most widely used analysis methods for progressive failure of composite …