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Showing 1 to 3 of 3 for “"fuselage frame"”.

  1. 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 …

    vt Repository record for Impact Response and Failure of a Textile Composite Fuselage Frame (opens in a new tab)

  2. 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 …

    vt Repository record for Development of a Progressive Failure Finite Element Analysis For a Braided Composite Fuselage Frame (opens in a new tab)

  3. 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 …

    vt Repository record for Optimal design of composite fuselage frames for crashworthiness (opens in a new tab)