1. Article › Scientific › Peer-reviewed
  2. A fast procedure for the design of composite stiffened panels

    Bisagni, C. & Vescovini, R., 2015, In : The Aeronautical Journal. 119, 1212, p. 185-201 17 p.

    Research output: Contribution to journalArticleScientificpeer-review

  3. A procedure for the evaluation of damping effects in composite laminated structures

    Vescovini, R. & Bisagni, C., 2015, In : Progress in Aerospace Sciences. 78, October, p. 19-29 11 p.

    Research output: Contribution to journalArticleScientificpeer-review

  4. An experimental vibration-buckling investigation on classical and variable angle tow composite shells under axial compression

    Labans, E., Abramovich, H. & Bisagni, C., 9 Jun 2019, In : Journal of Sound and Vibration. 449, p. 315-329 15 p.

    Research output: Contribution to journalArticleScientificpeer-review

  5. Assessment of dynamic effects on aircraft design loads: The landing impact case

    Bronstein, M., Feldman, E., Vescovini, R. & Bisagni, C., 2015, In : Progress in Aerospace Sciences. 78, October, p. 131-139 9 p.

    Research output: Contribution to journalArticleScientificpeer-review

  6. Behavior of curved laminated composite panels and shells under axial compression

    Abramovich, H. & Bisagni, C., 2015, In : Progress in Aerospace Sciences. 78, October, p. 74-106 33 p.

    Research output: Contribution to journalArticleScientificpeer-review

  7. Bending of Composite Cylindrical Shells with Circular Cutouts: Experimental Validation

    Labans, E., Bisagni, C., Celebi, M., Tatting, B., Gürdal, Z., Blom-Schieber, A., Rassaian, M. & Wanthal, S., 2019, In : Journal of Aircraft: devoted to aeronautical science and technology. 56, 4, p. 1534-1550 17 p.

    Research output: Contribution to journalArticleScientificpeer-review

  8. Buckling and free vibration study of variable and constant-stiffness cylindrical shells

    Labans, E. & Bisagni, C., 15 Feb 2019, In : Composite Structures. 210, p. 446-457 12 p.

    Research output: Contribution to journalArticleScientificpeer-review

  9. Composite cylindrical shells under static and dynamic axial loading: An experimental campaign

    Bisagni, C., 2015, In : Progress in Aerospace Sciences. 78, October, p. 107-115 9 p.

    Research output: Contribution to journalArticleScientificpeer-review

  10. Dynamic finite element simulations of composite stiffened panels with a transverse-isotropic viscoelastic energy dissipation model

    Ludwig, T., Doreille, M., Merazzi, S., Vescovini, R. & Bisagni, C., 2015, In : Progress in Aerospace Sciences. 78, October, p. 30-38 9 p.

    Research output: Contribution to journalArticleScientificpeer-review

  11. Experimental investigation and numerical simulation of unidirectional carbon fiber composite under multi-axial loadings

    Qiao, Y., Bisagni, C. & Bai, Y., 1 Sep 2017, In : Composites Part B: Engineering. 124, p. 190-206 17 p.

    Research output: Contribution to journalArticleScientificpeer-review

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