1. 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

  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. 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

  5. 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

  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 Postbuckling Analysis of Composite-Stiffened Panels Using a Semi-Analytical Approach

    Vescovini, R. & Bisagni, C., 2018, Buckling and Postbuckling Structures II: Experimental, Analytical and Numerical Studies. Falzon, B. G. & Aliabadi, M. H. F. (eds.). World Scientific, Vol. 9. p. 173-207 35 p. (Computational and Experimental Methods in Structures).

    Research output: Chapter in Book/Report/Conference proceedingChapterScientificpeer-review

  10. 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

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