1. 2019
  2. 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

  3. A polymorphic element formulation towards multiscale modelling of composite structures

    Kocaman, E. S., Chen, B. Y. & Pinho, S. T., 1 Apr 2019, In : Computer Methods in Applied Mechanics and Engineering. 346, p. 359-387 29 p.

    Research output: Contribution to journalArticleScientificpeer-review

  4. 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

  5. ES-PIM applied to buckling of variable angle tow laminates

    Giovani Pereira Castro, S., Donadon, M. V. & Guimarães, T. A. M., 1 Feb 2019, In : Composite Structures. 209, p. 67-78 12 p.

    Research output: Contribution to journalArticleScientificpeer-review

  6. On cohesive element parameters and delamination modelling

    Lu, X., Ridha, M., Chen, B. Y., Tan, V. B. C. & Tay, T. E., 1 Feb 2019, In : Engineering Fracture Mechanics. 206, p. 278-296 19 p.

    Research output: Contribution to journalArticleScientificpeer-review

  7. Preliminary aeroelastic design of composite wings subjected to critical gust loads

    Rajpal, D., Gillebaart, E. & De Breuker, R., 1 Feb 2019, In : Aerospace Science and Technology. 85, p. 96-112 17 p.

    Research output: Contribution to journalArticleScientificpeer-review

  8. 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

  9. Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings

    Roessler, C., Stahl, P., Sendner, F., Hermanutz, A., Sodja, J., De Breuker, R., Koimtzoglou, C., Kotinis, D., Georgopoulos, P. & More Authors, 2019, AIAA Scitech 2019 Forum: 7-11 January 2019, San Diego, California, USA. 20 p. AIAA 2019-1813

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

  10. Fast Aeroelastic Analysis and Optimisation of Large Mixed Materials Wind Turbine Blades

    Hegberg, T., 2019, 159 p.

    Research output: ThesisDissertation (TU Delft)Scientific

  11. Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion

    Wang, X., van Kampen, E-J., Chu, Q. & De Breuker, R., 2019, In : Journal of Guidance, Control, and Dynamics: devoted to the technology of dynamics and control. 18 p.

    Research output: Contribution to journalArticleScientificpeer-review

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