1. 2015
  2. Overview of the DAEDALOS project

    Bisagni, C., 2015, In : Progress in Aerospace Sciences. 78, October, p. 1-7 7 p.

    Research output: Contribution to journalArticleScientificpeer-review

  3. Semi-analytical buckling analysis of omega stiffened panels under multi-axial loads

    Vescovini, R. & Bisagni, C., 2015, In : Composite Structures. 120, February, p. 285-299 15 p.

    Research output: Contribution to journalArticleScientificpeer-review

  4. Special Issue: DAEDALOS - Dynamics in Aircraft Engineering Design and Analysis for Light Optimized Structures

    Bisagni, C., 2015, In : Progress in Aerospace Sciences. 78, p. 1-140

    Research output: Contribution to journalSpecial issueScientific

  5. Stacking sequence influence on imperfection sensitivity of cylindrical composite shells under axial compression

    Friedrich, L., Loosen, S., Liang, K., Ruess, M., Bisagni, C. & Schroder, KU., 2015, In : Composite Structures. 134, December, p. 750-761 12 p.

    Research output: Contribution to journalArticleScientificpeer-review

  6. Static and dynamic buckling of a DAEDALOS composite panel including material damping

    Dalenbring, M., Falk, U., Zdunek, A., Vescovini, R. & Bisagni, C., 2015, Proceedings of the 56th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference. s.n. (ed.). Reston: American Institute of Aeronautics and Astronautics Inc. (AIAA), p. 1-14 14 p.

    Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientific

  7. 2016
  8. 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/Conference proceedings/Edited volumeConference contributionScientificpeer-review

  9. Buckling tests of sandwich cylindrical shells with and without cut-outs

    Bisagni, C., 2016, Proceedings of American Society for Composites: 31st Technical Conference and ASTM Committee D30 Meeting, Williamsburg, Virginia, USA. Davidson, B. D., Czabaj, M. W. & Ratcliffe, J. G. (eds.). 10 p.

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

  10. Chaos Theory applied to buckling analysis of composite cylindrical shell

    Alfano, M. & Bisagni, C., 2016, Proceedings of 30th Congress of International Council of the Aeronautical Sciences: Daejeon, South Korea. 8 p. 673

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

  11. 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

  12. 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

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