1. 2020
  2. Parametric studies on the dynamic buckling phenomenon of a composite cylindrical shell under impulsive axial compression

    Zaczynska, M., Abramovich, H. & Bisagni, C., 15 Sep 2020, In : Journal of Sound and Vibration. 482, 17 p., 115462.

    Research output: Contribution to journalArticleScientificpeer-review

  3. 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

  4. 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

  5. Numerical study of quasi-static and fatigue delamination growth in a post-buckled composite stiffened panel

    Raimondo, A., Doesburg, S. A. & Bisagni, C., 1 Feb 2020, In : Composites Part B: Engineering. 182, 12 p., 107589.

    Research output: Contribution to journalArticleScientificpeer-review

  6. A Methodology to Investigate Skin-Stringer Separation in Postbuckled Composite Stiffened Panels

    Kootte, L. & Bisagni, C., 2020, AIAA Scitech 2020 Forum: 6-10 January 2020, Orlando, FL. American Institute of Aeronautics and Astronautics Inc. (AIAA), 14 p. AIAA 2020-0477

    Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

  7. 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

  8. Buckling of 3D-Printed Cylindrical Shells with Corrugated Surface

    Labans, E. & Bisagni, C., 2020, AIAA Scitech 2020 Forum: 6-10 January 2020, Orlando, FL. American Institute of Aeronautics and Astronautics Inc. (AIAA), 11 p. AIAA 2020-1925

    Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

  9. Scaling Methodology Applied to Buckling of Sandwich Composite Cylindrical Shells

    Uriol Balbin, I., Bisagni, C., Schultz, M. R. & Hilburger, M. W., 2020, In : AIAA Journal: devoted to aerospace research and development. 10 p.

    Research output: Contribution to journalArticleScientificpeer-review

  10. 2019
  11. 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

  12. Geometrically nonlinear finite element model for predicting failure in composite structures

    Patni, M., Minera, S., Bisagni, C., Weaver, P. M. & Pirrera, A., 1 Oct 2019, In : Composite Structures. 225, 111068.

    Research output: Contribution to journalArticleScientificpeer-review

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