1. 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. AIAA, 14 p. AIAA 2020-0477

    Research output: Chapter in Book/Report/Conference proceedingConference contributionScientificpeer-review

  2. A Numerical Approach for the Evaluation of the Local Stress Ratio in Fatigue-Driven Delamination Analysis

    Raimondo, A. & Bisagni, C., 2019, AIAA Scitech 2019 Forum: 7-11 January 2019, San Diego, California, USA. 13 p. AIAA 2019-1545

    Research output: Chapter in Book/Report/Conference proceedingConference contributionScientificpeer-review

  3. 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

  4. 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

  5. A study of the dynamic effects on the design loads of a civil aircraft

    Bronstein, M., Feldman, E., Vescovini, R. & Bisagni, C., 2016, Proceedings of 56th Israel Annual Conference on Aerospace Sciences: Tel-Aviv & Haifa, Israel. 11 p.

    Research output: Chapter in Book/Report/Conference proceedingConference contributionScientificpeer-review

  6. 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

  7. Analysis and testing of a thermoplastic composite stiffened panel under compression

    van Dooren, K., Labans, E., Tijs, B., Bisagni, C. & Waleson, J., 2019, Proceedings of 22nd International Conference on Composite Materials (ICCM22), Melbourne, AU, August 11-16, 2019. 7 p. 5108-2

    Research output: Chapter in Book/Report/Conference proceedingConference contributionScientific

  8. 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

  9. Artificial Intelligence techniques in design optimization of variable stiffness cylindrical shells

    Pitton, S., Ricci, S. & Bisagni, C., 2019, Proceedings of Italian Association of Aeronautics and Astronautics, XXV International Congress, 9-12 September 2019, Rome, Italy. p. 1197-2004

    Research output: Chapter in Book/Report/Conference proceedingConference contributionScientific

  10. 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

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