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. Analysis of Local Stress Ratio for Delamination in Composites Under Fatigue Loads

    Raimondo, A. & Bisagni, C., 2020, In : AIAA Journal: devoted to aerospace research and development. 58, 1, p. 455-463 10 p.

    Research output: Contribution to journalArticleScientificpeer-review

  6. 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

  7. 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

  8. 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

  9. 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

  10. Buckling optimization of variable stiffness cylindrical shells through artificial intelligence techniques

    Pitton, S. F., Ricci, S. & Bisagni, C., 15 Dec 2019, In : Composite Structures. 230, 9 p., 111513.

    Research output: Contribution to journalArticleScientificpeer-review

  11. Closed-form solutions for thermomechanical buckling of orthotropic composite plates

    Gutiérrez Álvarez, J. & Bisagni, C., 1 Feb 2020, In : Composite Structures. 233, 7 p., 111622.

    Research output: Contribution to journalArticleScientificpeer-review

  12. 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

  13. 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

  14. 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

  15. Experimental investigation of reinforced bonded joints for composite laminates

    Bisagni, C., Furfari, D. & Pacchione, M., 1 Feb 2018, In : Journal of Composite Materials. 52, 4, p. 431-447 17 p.

    Research output: Contribution to journalArticleScientificpeer-review

  16. Experimental validation of the vibration correlation technique robustness to predict buckling of unstiffened composite cylindrical shells

    Franzoni, F., Odermann, F., Lanbans, E., Bisagni, C., Andrés Arbelo, M. & Degenhardt, R., 15 Sep 2019, In : Composite Structures. 224, 9 p., 111107.

    Research output: Contribution to journalArticleScientificpeer-review

  17. Fast analysis of non-symmetric panels using semi-analytical techniques

    Vescovini, R. & Bisagni, C., 2016, In : Composites Part B: Engineering. 99, p. 48-62

    Research output: Contribution to journalArticleScientificpeer-review

  18. Fatigue analysis of a post-buckled composite single-stringer specimen taking into account the local stress ratio

    Raimondo, A. & Bisagni, C., 15 Jul 2020, In : Composites Part B: Engineering. 193, 108000.

    Research output: Contribution to journalArticleScientificpeer-review

  19. Fatigue life and damage tolerance of postbuckled composite stiffened structures with indentation damage

    Dávila, C. G. & Bisagni, C., 1 Mar 2018, In : Journal of Composite Materials. 52, 7, p. 931-943 13 p.

    Research output: Contribution to journalArticleScientificpeer-review

  20. Fatigue life and damage tolerance of postbuckled composite stiffened structures with initial delamination

    Davila, C. & Bisagni, C., 2016, In : Composite Structures. 161, p. 73-84

    Research output: Contribution to journalArticleScientificpeer-review

  21. Flexural behavior of sandwich panels with cellular wood, plywood stiffener/foam and thermoplastic composite core

    Labans, E., Kalnins, K. & Bisagni, C., 24 Mar 2017, In : Journal of Sandwich Structures & Materials. 21 (2019), 2, p. 784-805 22 p.

    Research output: Contribution to journalArticleScientificpeer-review

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