1. 2016
  2. Multi-scale analysis and optimisation of three-dimensional woven composite structures combining response surface method and genetic algorithms

    Fu, X., Ricci, S. & Bisagni, C., 2016, In : CEAS Aeronautical Journal. 8, 1, p. 129-141 13 p.

    Research output: Contribution to journalArticleScientificpeer-review

  3. On the structural design of imperfection sensitive laminated composite shell structures subjected to axial compression

    Friedrich, L., Lyssakow, P., Pearce, G., Ruess, M., Bisagni, C. & Schroder, KU., 2016, Proceedings of ECCOMAS Congress 2016, VII European Congress on Computational Methods in Applied Sciences and Engineering: Crete Island, Greece. 8 p.

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

  4. Parametric bird strike study of a transonic rotor using isogeometric analysis

    Duckitt, S., Bisagni, C. & Shahpar, S., 2016, Proceedings of ASME Turbo Expo 2016: Turbomachinery Technical Conference & Exposition, Seoul, South Korea. 11 p. GT2016-57464

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

  5. 2015
  6. 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

  7. 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

  8. 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

  9. 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

  10. 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

  11. 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

  12. Effect of buckling modes on the fatigue life and damage tolerance of stiffened structures

    Davila, CG., Bisagni, C. & Rose, C., 2015, Proceedings of the 56th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference. s.n. (ed.). Reston: AIAA, p. 1-9 9 p.

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

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