If you made any changes in Pure these will be visible here soon.

Research Output

2020

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. American Institute of Aeronautics and Astronautics Inc. (AIAA), 14 p. AIAA 2020-0477

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

Open Access
File
61 Downloads (Pure)

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

Open Access
File
66 Downloads (Pure)

Buckling of 3D-Printed Cylindrical Shells with Corrugated Surface

Labans, E. & Bisagni, C., 2020, AIAA Scitech 2020 Forum: 6-10 January 2020, Orlando, FL. American Institute of Aeronautics and Astronautics Inc. (AIAA), 11 p. AIAA 2020-1925

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

Open Access
File
53 Downloads (Pure)

Closed-form solutions for thermomechanical buckling of orthotropic composite plates

Gutiérrez Álvarez, J. & Bisagni, C., 1 Feb 2020, In : Composite Structures. 233, 7 p., 111622.

Research output: Contribution to journalArticleScientificpeer-review

Fatigue analysis of a post-buckled composite single-stringer specimen taking into account the local stress ratio

Raimondo, A. & Bisagni, C., 15 Jul 2020, In : Composites Part B: Engineering. 193, 108000.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
1 Citation (Scopus)
31 Downloads (Pure)

Numerical study of quasi-static and fatigue delamination growth in a post-buckled composite stiffened panel

Raimondo, A., Doesburg, S. A. & Bisagni, C., 1 Feb 2020, In : Composites Part B: Engineering. 182, 12 p., 107589.

Research output: Contribution to journalArticleScientificpeer-review

2 Citations (Scopus)

Parametric studies on the dynamic buckling phenomenon of a composite cylindrical shell under impulsive axial compression

Zaczynska, M., Abramovich, H. & Bisagni, C., 15 Sep 2020, In : Journal of Sound and Vibration. 482, 17 p., 115462.

Research output: Contribution to journalArticleScientificpeer-review

1 Citation (Scopus)

Scaling Methodology Applied to Buckling of Sandwich Composite Cylindrical Shells

Uriol Balbin, I., Bisagni, C., Schultz, M. R. & Hilburger, M. W., 1 Jan 2020, In : AIAA Journal: devoted to aerospace research and development. 58, 8, p. 3680-3689 10 p.

Research output: Contribution to journalArticleScientificpeer-review

2019

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/Conference proceedings/Edited volumeConference contributionScientific

Open Access
File
40 Downloads (Pure)

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

11 Citations (Scopus)

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/Conference proceedings/Edited volumeConference contributionScientificpeer-review

Open Access
File
79 Downloads (Pure)

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/Conference proceedings/Edited volumeConference contributionScientific

Open Access
File
21 Downloads (Pure)

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

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

14 Citations (Scopus)

Buckling optimization of variable stiffness cylindrical shells through artificial intelligence techniques

Pitton, S. F., Ricci, S. & Bisagni, C., 15 Dec 2019, In : Composite Structures. 230, 9 p., 111513.

Research output: Contribution to journalArticleScientificpeer-review

2 Citations (Scopus)

Experimental validation of the vibration correlation technique robustness to predict buckling of unstiffened composite cylindrical shells

Franzoni, F., Odermann, F., Lanbans, E., Bisagni, C., Andrés Arbelo, M. & Degenhardt, R., 15 Sep 2019, In : Composite Structures. 224, 9 p., 111107.

Research output: Contribution to journalArticleScientificpeer-review

4 Citations (Scopus)

Fatigue crack propagation in composite laminates by a novel approach based on the S-N diagrams

Raimondo, A. & Bisagni, C., 2019, Proceedings of 22nd International Conference on Composite Materials (ICCM22), Melbourne, AU, August 11-16, 2019. 10 p. 4114-3

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

Open Access
File
28 Downloads (Pure)

Fatigue life of post-buckled composite structures

Bisagni, C., 2019, Proceedings of 22nd International Conference on Composite Materials (ICCM22), Melbourne, AU, August 11-16, 2019. 8 p.

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

Open Access
File
42 Downloads (Pure)

Geometrically nonlinear finite element model for predicting failure in composite structures

Patni, M., Minera, S., Bisagni, C., Weaver, P. M. & Pirrera, A., 1 Oct 2019, In : Composite Structures. 225, 111068.

Research output: Contribution to journalArticleScientificpeer-review

2 Citations (Scopus)
2018

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/Conference proceedings/Edited volumeChapterScientificpeer-review

Experimental investigation of reinforced bonded joints for composite laminates

Bisagni, C., Furfari, D. & Pacchione, M., 1 Feb 2018, In : Journal of Composite Materials. 52, 4, p. 431-447 17 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
2 Citations (Scopus)
59 Downloads (Pure)

Fatigue life and damage tolerance of postbuckled composite stiffened structures with indentation damage

Dávila, C. G. & Bisagni, C., 1 Mar 2018, In : Journal of Composite Materials. 52, 7, p. 931-943 13 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
6 Citations (Scopus)
36 Downloads (Pure)

Mechanical Response of Variable and Constant-Stiffness Cylindrical Shells for Launcher Structures

Labans, E. & Bisagni, C., 2018, ECSSMET 2018: 15th European Conference on Spacecraft Structures: 2018, Noordwijk, Netherlands. 5 p.

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

Open Access
File
35 Downloads (Pure)

Scaling methodology for buckling of sandwich composite cylindrical structures

Balbin, I. U., Bisagni, C., Schultz, M. R. & Hilburger, M. W., 2018, AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials. 210049 ed. American Institute of Aeronautics and Astronautics Inc. (AIAA), 14 p. AIAA 2018-1988

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

3 Citations (Scopus)

Skin-Stiffener Separation in T-Stiffened Composite Specimens in Postbuckling Condition

Zou, D. & Bisagni, C., 1 Jul 2018, In : Journal of Aerospace Engineering. 31, 4, 10 p., 04018027.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
3 Citations (Scopus)
120 Downloads (Pure)

Study of Skin-Stringer Separation in Postbuckled Composite Aeronautical Structures

Kootte, L., Bisagni, C., Davila, C. & Ranatunga, V., 2018, Proceedings of the American Society for Composites Thirty-third Technical Conference. p. 1750 - 1761

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

Open Access
File
13 Downloads (Pure)

Thermal-mechanical buckling of composite plates for aerospace applications

Gutierrez Alvarez, J. & Bisagni, C., 2018, Proceedings of the 18th European Conference on Composite Materials: 24-28th June 2018, Athens, Greece. 6 p.

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

Open Access
File
35 Downloads (Pure)

Virtual testing of thermoplastic composites: Towards a hybrid simulation-physical testing pyramid

Tijs, B., Lopes, CS., Turon, A., Bisagni, C., Waleson, J., van Ingen, J. W. & Veldman, S. L., 2018, Proceedings of the 18th European Conference on Composite Materials: 24-28th June 2018, Athens, Greece. Watkins, S. & Mohamed, A. (eds.). 6 p.

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

Open Access
File
184 Downloads (Pure)
2017

Experimental investigation and numerical simulation of unidirectional carbon fiber composite under multi-axial loadings

Qiao, Y., Bisagni, C. & Bai, Y., 1 Sep 2017, In : Composites Part B: Engineering. 124, p. 190-206 17 p.

Research output: Contribution to journalArticleScientificpeer-review

3 Citations (Scopus)

Fatigue simulation for damage propagation in composite structures

Di Memmo, I. & Bisagni, C., 1 Jan 2017, 32nd Technical Conference of the American Society for Composites 2017. Yu, W., Pipes, R. B. & Goodsell, J. (eds.). DEStech publications, Inc., Vol. 2. p. 1009-1019 11 p.

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

2 Citations (Scopus)

Flexural behavior of sandwich panels with cellular wood, plywood stiffener/foam and thermoplastic composite core

Labans, E., Kalnins, K. & Bisagni, C., 24 Mar 2017, In : Journal of Sandwich Structures & Materials. 21 (2019), 2, p. 784-805 22 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
9 Citations (Scopus)
196 Downloads (Pure)

Modelling strategies for numerical simulation of aircraft ditching

Bisagni, C. & Pigazzini, M. S., 1 May 2017, In : International Journal of Crashworthiness. p. 1-18 18 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
4 Citations (Scopus)
176 Downloads (Pure)

Probabilistic buckling analysis of sandwich composite cylindrical shells based on measured imperfections

Bisagni, C. & Alfano, M., 2017, 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference: Grapevine, USA. American Institute of Aeronautics and Astronautics Inc. (AIAA), 11 p. AIAA 2017-0886

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

5 Citations (Scopus)
2016

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

Open Access
File
75 Downloads (Pure)

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

Open Access
File
50 Downloads (Pure)

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

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

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

21 Citations (Scopus)

Fatigue life of postbuckled structures with indentation damage

Davila, CG. & Bisagni, C., 2016, Proceedings of the 17th European Conference on Composite Materials: Munich, Germany 2016. Reston, 9 p.

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

Open Access
File
23 Downloads (Pure)

Fatigue life of postbuckled structures with indentation damage

Davila, CG. & Bisagni, C., 2016, Proceedings of the 57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference. Reston: American Institute of Aeronautics and Astronautics Inc. (AIAA), 12 p. AIAA 2016-0982

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

Open Access

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

7 Citations (Scopus)

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/Conference proceedings/Edited volumeConference contributionScientificpeer-review

Open Access
File
174 Downloads (Pure)

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/Conference proceedings/Edited volumeConference contributionScientificpeer-review

2015

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

9 Citations (Scopus)

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

Open Access
11 Citations (Scopus)

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

Open Access
2 Citations (Scopus)

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

Open Access
13 Citations (Scopus)

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

Open Access
23 Citations (Scopus)

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

Open Access
6 Citations (Scopus)