Nombre de documents

98

CV de Michele D'Ottavio


Communication dans un congrès39 documents

  • M. D'Ottavio, L. Dozio, R. Vescovini, O. Polit. Mechanical response of composite plates by means of a Sublaminate Generalized Unified Formulation and Ritz solution. A.J.M. Ferreira and A.M.A. Neves and E. Viola and F. Tornabene and N. Fantuzzi. 2nd International Conference on Mechanics of Composites, 2016, Porto, Portugal. Esculapio, 2016, <10.15651/978-88-748-8963-1>. <hal-01367035>
  • O. Polit, M. D'Ottavio, P. Vidal. High-order plate/shell FE for piezoelectric analysis: the bimorph configuration. A.L. Araújo and C.A. Mota Soares. Proceedings of the 7th ECCOMAS Thematic Conference on Smart Structures and Materials (SMART2015), 2015, Ponte Delgada, Portugal. 2015. <hal-01367041>
  • M. D'Ottavio, O. Polit. Variable kinematics models for buckling and vibration of multilayered panels. A.J.M. Ferreira. 18th International Conference on Composite Structures, 2015, Lisbon, Portugal. 2015. <hal-01367040>
  • G. Giunta, S. Belouettar, O. Polit, L. Gallimard, P. Vidal, et al.. Analysis of three-dimensional beams via hierarchical finite elements and a proper generalized decomposition. 4th African Conference on Computational Mechanics, 2015, Marrakech, Morocco. 2015. <hal-01367039>
  • T. H. C. Le, M. D'Ottavio, P. Vidal, O. Polit. Numerical assessment of a new QC4 finite element for variable-kinematics composite plates. Seventh International Symposium on Design, Modelling and Experiments of Advanced Structures and Smart Systems (DeMEASS VI), 2015, Radebeul, Germany. 2015. <hal-01367037>
  • M. D'Ottavio, O. Polit. A Generalized Unified Formulation for vibration analysis of prestressed laminated panels. E. Carrera et al. Proceedings of the 23rd Conference of the Italian Association of Aeronautics and Astronautics (AIDAA 2015), 2015, Torino, Italy. 2015. <hal-01367036>
  • M. D'Ottavio, P. Vidal, O. Polit. Robust plate/shell finite element with Zig-Zag function for piezoelectric analysis. Sixth International Symposium on Design, Modelling and Experiments of Advanced Structures and Smart Systems (DeMEASS VI), 2014, Ede, The, Netherlands. 2014. <hal-01367045>
  • C. Wenzel, M. D'Ottavio, O. Polit, P. Vidal. Plate finite elements applied to the free-edge singularity in bending and extension. Sixth International Symposium on Design, Modelling and Experiments of Advanced Structures and Smart Systems (DeMEASS VI), 2014, Ede, The, Netherlands. 2014. <hal-01367044>
  • M. D'Ottavio, O. Polit. Refined 2D models for buckling and vibration of cylindrical sandwich shells. International Symposium on Dynamic Response and Failure of Composite Materials, 2014, Ischia, Italy. 2014. <hal-01367046>
  • M. D'Ottavio, C. Wenzel, P. Vidal, E. Valot, O. Polit. Free-edge stress fields in composite laminates: assessment of finite plate elements. A.J.M. Ferreira. 17th International Conference on Composite Structures, 2013, Porto, Portugal. 2013. <hal-01367056>
  • O. Polit, M. D'Ottavio, P. Vidal. Robust shell finite element for piezoelectric analysis. E. Carrera and M. Cinefra and F. Miglioretti and M. Petrolo. Proceedings of the 6th ECCOMAS Thematic Conference on Smart Structures and Materials (SMART2013), 2013, Torino, Italy. 2013. <hal-01367053>
  • C. Wenzel, M. D'Ottavio, P. Vidal, O. Polit. Heterogeneous kinematical analysis of beam structures via the Extended Variational Formulation. Fifth International Symposium on Design, Modelling and Experiments of Advanced Structures and Smart Systems (DeMEASS V), 2012, Ulrichsberg, Austria. 2012. <hal-01367061>
  • M. D'Ottavio, O. Polit. Quasi-3D solutions for sandwich buckling and wrinkling. A.~J.~M.~Ferreira and E.~Carrera. International Conference on Mechanics of Nano, Micro and Macro Composite Structures, 2012, Turin, Italy. 2012. <hal-01367059>
  • O. Polit, P. Vidal, M. D'Ottavio. Robust shell finite element for thin to very thick composite structures. A.J.M. Ferreira and E. Carrera. International Conference on Mechanics of Nano, Micro and Macro Composite Structures, 2012, Turin, Italy. 2012. <hal-01367065>
  • M. D'Ottavio, O. Polit. Assessment of Plate Models for Sandwich Bending, Global Buckling and Wrinkling. 10th International Conference on Sandwich Structures, 2012, Nantes, France. 2012. <hal-01367060>
  • N. D. Thai, J.-F. Caron, M. D'Ottavio. Benchmark d'un modèle pour sandwiches et multicouches, de type layerwise en contrainte. 17èmes Journées Nationales sur les Composites (JNC17), 2011, Poitiers, France. 2011. <hal-01367070>
  • O. Polit, P. Vidal, M. D'Ottavio. Seven parameters C⁰ F.E. for heterogeneous plate structures. A.J.M. Ferreira. 16th International Conference on Composite Structures, 2011, Porto, Portugal. 2011. <hal-01367067>
  • M. D'Ottavio, O. Polit, P. Vidal. Some benchmarks for assessing models for composite smart structures (Keynote Lecture). Fourth International Symposium on Design, Modelling and Experiments of Advanced Structures and Smart Systems (DeMEASS IV), 2011, Urspelt, Luxembourg. 2011. <hal-01367069>
  • M. D'Ottavio, O. Polit, E. Carrera. Assessment of models for the buckling analysis of composite plates and shells. A.J.M. Ferreira. 16th International Conference on Composite Structures, 2011, Porto, Portugal. 2011. <hal-01367068>
  • D.T. Nguyen, Jean-François Caron, M. D'Ottavio. Benchmark d'un modele pour sandwiches et multicouches, de type layer-wise en contrainte. AMAC. 17èmes Journées Nationales sur les Composites (JNC17), Jun 2011, Poitiers-Futuroscope, France. pp.165, 2011. <hal-00597054v2>
  • Philippe Vidal, Michele D Ottavio, Olivier Polit. Un E.F. C0 basé sur un modèle raffiné pour l'analyse multi-physique de plaques hétérogènes. 10e colloque national en calcul des structures, May 2011, Giens, France. pp.Clé USB, 2011. <hal-00592860>
  • P. Vidal, M. D'Ottavio, O. Polit. Un E.F. C⁰ basé sur un modèle raffiné pour l'analyse multyphysique de plaques hétérogènes. 10e Colloque National en Calcul des Structures, 2011, Giens, France. 2011. <hal-01367071>
  • O. Polit, P. Vidal, M. D'Ottavio. A new C⁰ finite element based on a refined theory for multifield analysis of heterogeneous plate/shell structures. IV European Conference on Computational Mechanics, 2010, Paris, France. 2010. <hal-01367074>
  • E. Valot, O. Polit, M. D'Ottavio, P. Vidal. Influence of 2D finite element models on the 3D stresses evaluation for composite laminates: assessment of anisotropic effects. IV European Conference on Computational Mechanics, 2010, Paris, France. 2010. <hal-01367075>
  • M. D'Ottavio, S. Brischetto, O. Polit. Hierarchic 2D Models for Piezoelectric Sandwich Shells. B.A. Schrefler and U. Perego. 8th World Congress on Computational Mechanics (WCCM8), 2008, Venice, Italy. 2008. <hal-01367078>
  • M. D'Ottavio, O. Polit. Sensititvity analysis of thickness assumptions for axiomatic 2D models of linear elastic and piezoelectric laminates. Second International Symposium on Design, Modelling and Experiments of Adaptive Structures and Smart Systems (DeMEASS II), 2007, Bad Herrenalb, Germany. 2007. <hal-01367081>
  • M. D'Ottavio, B. Kröplin. Two-dimensional axiomatic modeling of piezoelectric panels. First International Symposium on Design, Modelling and Experiments of Adaptive Structures and Smart Systems (DeMEASS I), 2006, Bardonecchia, Italy. 2006. <hal-01367084>
  • M. D'Ottavio, F. K. Wittel, B. Kröplin. An Open Toolbox for Damage Simulation. Online Proceedings of CDCM 2006 - Conference on Damage in Composite Materials 2006, 2006, Stuttgart, Germany. 2006. <hal-01367090>
  • T. Wallmersperger, F. K. Wittel, M. D'Ottavio, B. Kröplin. Multiscale modelling of polymer gels. First International Symposium on Design, Modelling and Experiments of Adaptive Structures and Smart Systems (DeMEASS I), 2006, Bardonecchia, Italy. 2006. <hal-01367085>
  • E. Carrera, M. Boscolo, C. Fagiano, A. Robaldo, M. D'Ottavio. Mixed Finite Elements for Piezoelectric Plates based on a Unified Formulation. C. Borri and L. Facchini and G. Federici and M. Primicerio. 17th Conference of the Italian Association for Theoretical and Applied Mechanics (AIMETA 2005), 2005, Florence, Italy. Firenze University Press, 2005. <hal-01367093>
  • H. Haque, I. Kolaric, U. Vohrer, T. Wallmersperger, M. D'Ottavio, et al.. Multi-Walled Carbon-Nanotubes-Sheet Actuators: Theoretical and Experimental Investigations. Y. Bar-Cohen. SPIE Proceedings of Smart Structures and Materials 2005: Electroactive Polymer Actuators and Devices, 2005, San Diego, CA, United States. 5759, pp.203-213, 2005. <hal-01367091>
  • M. Waedt, M. D'Ottavio, T. Wallmersperger, B. Kröplin, K. Wolf, et al.. Kriterien zur Bewertung des Mappings von Umform- auf Crashsimulation. 3. LS-DYNA User's Conference, 2004, Bamberg, Germany. 2004. <hal-01367095>
  • M. D'Ottavio. Extension of Reissner's Mixed variational Theorem to Piezoelectric Laminates. 2nd Meeting CIMNE-ISD Researchers, 2004, Barcelona, Spain. 2004. <hal-01367098>
  • T. Wallmersperger, M. D'Ottavio, B. Kröplin, R. W. Gülch. On the Modelling of Electroactive Polymers. 14th Congress of the European Society of Biomechanics (ESB), 2004, s Hertogenbosch, The, Netherlands. 2004. <hal-01367097>
  • M. D'Ottavio, G. F. Ferraris, E. Koray, N. Topcu, K. Eberle, et al.. Determination of the Plastic Anisotropy of Metals by Indentation Tests. Part A: Numerical and Experimental Analysis of Indentation. 4th ICFG Workshop on Process Simulation in the Metal Forming Industry, 2004, Shanghai, China. 2004. <hal-01367096>
  • D. Ballhause, M. D'Ottavio, E. Carrera. Partially mixed multilayered theories for piezoelectric plates. E.A. Lipitakis. Proceedings of the Sixth Hellenic-European Conference on Computer Mathematics and its Applications (HERCMA 2003), 2003, Athens, Hellas, Unknown or Invalid Region. LEA Publishers, 1, pp.153-163, 2003. <hal-01367099>
  • M. D'Ottavio, T. Wallmersperger, B. Kröplin, B. A. Grohmann. Coupled Numerical Aero-Servo-Elastic Simulation of Adaptive Helicopter Airfoils in Transonic Flow. H. A. Mang and F. G. Rammerstorfer and J. Eberhardsteiner. Proceedings of the Fifth World Congress on Computational Mechanics (WCCM V), 2002, Vienna, Austria. Vienna University of Technology, 2002. <hal-01367100>
  • T. Wallmersperger, M. D'Ottavio, B. Kröplin, R. W. Gülch. Coupled Multi-Field Formulation for Ionic Polymer Gels. H. A. Mang and F. G. Rammerstorfer and J. Eberhardsteiner. Proceedings of the Fifth World Congress on Computational Mechanics (WCCM V), 2002, Vienna, Austria. Vienna University of Technology, 2002. <hal-01367101>
  • B. A. Grohmann, P. Jänker, M. D'Ottavio, B. Kröplin, E. Carrera. Numerical Simulation of the Piezo-Aero-Elasticity of Smart Rotor Blades in Transonic Flow. K.J. Bathe. Proceedings of the First MIT Conference on Computational Fluid and Solid Mechanics, 2001, Cambridge, MA, United States. Elsevier, 2001. <hal-01367102>

Article dans une revue48 documents

  • M. D'Ottavio. A Sublaminate Generalized Unified Formulation for the analysis of composite structures and its application to sandwich plates bending. ComposStruct, 2016, 142, pp.187-199. <10.1016/j.compstruct.2016.01.087>. <hal-01367031>
  • G. Giunta, S. Belouattar, O. Polit, L. Gallimard, P. Vidal, et al.. Hierarchical beam finite elements based upon a variables separation method.. Int. J. Applied Mechanics, 2016, 8 (2), pp.1650026-35. <hal-01366955>
  • G. Giunta, S. Belouettar, O. Polit, L. Gallimard, P. Vidal, et al.. Hierarchical beam finite elements based upon a variables separation method. Int. J. of Applied Mechanics, 2016, to appear. <hal-01366900>
  • G. Giunta, S. Belouettar, O. Polit, L. Gallimard, P. Vidal, et al.. Hierarchical Beam Finite Elements Based Upon a Variables Separation Method. International Journal of Applied Mechanics, 2016, 8 (2), pp.1650026. <10.1142/S1758825116500265>. <hal-01367029>
  • C. Wenzel, M. D'Ottavio, O. Polit, P. Vidal. Assessment of free-edge singularities in composite laminates using higher-order plate elements.. Mechanics of Advanced Materials and Structures, Taylor & Francis, 2016, 23 (9), pp.948--959. <hal-01366954>
  • C. Wenzel, M. D'Ottavio, O. Polit, P. Vidal. Assessment of free-edge singularities in composite laminates using higher-order plate elements. Mechanics of Advanced Materials and Structures, Taylor & Francis, 2016, 23 (9), pp.948-959. <10.1080/15376494.2015.1121526>. <hal-01367030>
  • C. Wenzel, M. D'Ottavio, O. Polit, P. Vidal. Assessment of free-edge singularities in composite laminates using higher-order plate elements. Mechanics of Advanced Materials and Structures, Taylor & Francis, 2016, to appear. <hal-01366897>
  • M. D'Ottavio, O. Polit, W. Ji, A. M. Waas. Benchmark solutions and assessment of variable kinematics models for global and local buckling of sandwich struts. Composite Structures, Elsevier, 2016, <10.1016/j.compstruct.2016.01.019>. <hal-01367034>
  • O. Polit, M. D'Ottavio, P. Vidal. High-order plate finite elements for smart structure analysis. Composite Structures, Elsevier, 2016, 151, pp.81-90. <10.1016/j.compstruct.2016.01.092>. <hal-01367033>
  • M. D'Ottavio, L. Dozio, R. Vescovini, O. Polit. Bending analysis of composite laminated and sandwich structures using sublaminate variable-kinematic Ritz models. Composite Structures, Elsevier, 2016, 155, pp.45-62. <10.1016/j.compstruct.2016.07.036>. <hal-01367032>
  • O. Polit, M. D'Ottavio, P. Vidal. High-order plate finite elements for smart structure analysis. Composite Structures, Elsevier, 2016, 151, pp.81-90. <hal-01366898>
  • M. D'Ottavio, O. Polit, W. Ji, A.M. Waas. Benchmark solutions and assessment of variable kinematics models for global and local buckling of sandwich struts. Composite Structures, Elsevier, 2016, to appear. <hal-01366896>
  • O. Polit, M. D'Ottavio, P. Vidal. High-order plate finite elements for smart structure analysis.. Composite Structures, Elsevier, 2016, 151, pp.81--90. <hal-01366951>
  • M. Petrolo, E. Carrera, G. Iuso, C. De Visser, C. Patek, et al.. Further results on the aerodynamics and flight mechanics of a novel VTOL aircraft, the Anuloid. Int. J. of Aeronautical and Space Sciences, 2015, submitted. <hal-01366901>
  • O. Polit, L. Gallimard, P. Vidal, M. D'Ottavio, G. Giunta, et al.. An analysis of composite beams by means of hierarchical finite elements and a variables separation method. Computers and Structures, Elsevier, 2015, 158, pp.15 - 29. <10.1016/j.compstruc.2015.05.033>. <hal-01367038>
  • O. Polit, L. Gallimard, P. Vidal, M. D'Ottavio, G. Giunta, et al.. An analysis of composite beams by means of hierarchical finite elements and a variables separation method.. Computers and Structures, Elsevier, 2015, 158, pp.15--29. <hal-01366959>
  • O. Polit, L. Gallimard, P. Vidal, M. D'Ottavio, G. Giunta, et al.. An analysis of composite beams by means of hierarchical finite elements and a variables separation method. Computers and Structures, Elsevier, 2015, 158, pp.15 - 29. <hal-01366902>
  • M. D'Ottavio, O. Polit. Linearized global and local buckling analysis of sandwich struts with a refined quasi-3D model. Acta Mechanica, Springer Verlag, 2014, 225 (6). <hal-01366909>
  • M. D'Ottavio, O. Polit. Linearized global and local buckling analysis of sandwich struts with a refined quasi-3D model. Acta Mechanica, Springer Verlag, 2014, 225 (6), pp.81-101. <10.1007/s00707-014-1169-2>. <hal-01367047>
  • M. Petrolo, E. Carrera, M. D'Ottavio, C. De Visser, C. Pàtek, et al.. On the development of the Anuloid, a disk-shaped VTOL aircraft for urban areas. Advances in Aircraft and Spacecraft Science, Techno-Press, 2014, 1 (3), pp.353-378. <10.12989/aas.2014.1.3.353>. <hal-01367052>
  • P. Vidal, O. Polit, M. D'Ottavio, E. Valot. Assessment of the refined sinus plate finite element: Free edge effect and Meyer-Piening sandwich test. Finite Elements in Analysis and Design, Elsevier, 2014, 92, pp.60 - 71. <hal-01366910>
  • P. Vidal, O. Polit, M. D'Ottavio, E. Valot. Assessment of the refined sinus plate finite element: free edge effect and Meyer-Piening sandwich test.. Finite Elements in Analysis and Design, Elsevier, 2014, 92, pp.60--71. <hal-01366962>
  • P. Vidal, O. Polit, M. D'Ottavio, E. Valot. Assessment of the refined sinus plate finite element: Free edge effect and Meyer-Piening sandwich test. Finite Elements in Analysis and Design, Elsevier, 2014, 92, pp.60 - 71. <10.1016/j.finel.2014.08.004>. <hal-01367050>
  • C. Wenzel, P. Vidal, M. D'Ottavio, O. Polit. Coupling of heterogeneous kinematics and Finite Element approximations applied to composite beam structures. Composite Structures, Elsevier, 2014, 116, pp.177 - 192. <10.1016/j.compstruct.2014.04.022>. <hal-01367042>
  • C. Wenzel, P. Vidal, M. D'Ottavio, O. Polit. Coupling of heterogeneous kinematics and Finite Element approximations applied to composite beam structures. Composite Structures, Elsevier, 2014, 116, pp.177 - 192. <hal-01366965>
  • C. Wenzel, P. Vidal, M. D'Ottavio, O. Polit. Coupling of heterogeneous kinematics and Finite Element approximations applied to composite beam structures. Composite Structures, Elsevier, 2014, 116, pp.177 - 192. <hal-01366908>
  • M. D'Ottavio, P. Vidal, E. Valot, O. Polit. Assessment of Plate Theories for Free-Edge Effects.. Composite Part B : Eng. J., 2013, 48, pp.111--121. <hal-01366970>
  • M. D'Ottavio, P. Vidal, E. Valot, O. Polit. Assessment of Plate Theories for Free-Edge Effects. Composites Part B, 2013, 48, pp.111-121. <hal-01366913>
  • N. D. Thai, M. D'Ottavio, J.-F. Caron. Bending analysis of laminated and sandwich plates using a layer-wise stress model. Composite Structures, Elsevier, 2013, 96, pp.135-142. <10.1016/j.compstruct.2012.08.032>. <hal-01367055>
  • D.T. Nguyen, Michele D'Ottavio, Jean-François Caron. Bending analysis of laminated and sandwich plates using a layer-wise stress model. Composite Structures, Elsevier, 2013, 96, pp.135-142. <hal-00793355>
  • M. D'Ottavio, P. Vidal, E. Valot, O. Polit. Assessment of Plate Theories for Free-Edge Effects. Composites Part B: Engineering, Elsevier, 2013, 48, pp.111-121. <10.1016/j.compositesb.2012.12.007>. <hal-01367054>
  • Duc Thaï Nguyen, Michele D'Ottavio, Jean-François Caron. Benchmark d'un modèle pour sandwiches et multicouches, de type layerwise en contrainte. Annales de Chimie: Science des Materiaux, 2012, 37 (2-4), pp.445-456. <10.3166/rcma.22.445-456>. <hal-01157374>
  • O. Polit, P. Vidal, M. D'Ottavio. Robust C⁰ high-order plate finite element for thin to very thick structures: Mechanical and thermo-mechanical analysis. International Journal for Numerical Methods in Engineering, Wiley, 2012, 90, pp.429-451. <10.1002/nme.3328>. <hal-01367062>
  • O. Polit, P. Vidal, M. D'Ottavio. Robust C^0 high-order plate finite element for thin to very thick structures: mechanical and thermo-mecanical analysis. International Journal for Numerical Methods in Engineering, Wiley, 2012, 90 (4), pp.429-451. <hal-01366921>
  • O. Polit, P. Vidal, M. D'Ottavio. Robust C⁰ high-order plate finite element for thin to very thick structures: mechanical and thermo-mechanical analysis.. Int. J. of Numerical Methods in Engineering, 2012, 40, pp.429--451. <hal-01366972>
  • N. D. Thai, M. D'Ottavio, J.-F. Caron. Benchmark d'un modèle pour sandwiches et multicouches, de type layerwise en contrainte. Revue des composites et des matériaux avancés, 2012, 22 (3), pp.445-456. <hal-01367063>
  • P. Vidal, M. D'Ottavio, M. Ben Thaier, O. Polit. An efficient finite shell element for the static response of piezoelectric laminates.. J. of Intelligent Material Systems and Structures, 2011, 22 (7), pp.671--690. <hal-01366976>
  • P. Vidal, M. D'Ottavio, M. Ben Tha\"ier, O. Polit. An efficient shell finite element for the static response of piezoelectric laminates. Journal of Intelligent Material Systems and Structures, SAGE Publications (UK and US), 2011, 22 (7), pp.671-690. <hal-01366926>
  • P. Vidal, M. D'Ottavio, M. Ben Tha\"ıer, O. Polit. An efficient finite shell element for the static response of piezoelectric laminates. Journal of Intelligent Material Systems and Structures, SAGE Publications (UK and US), 2011, 22 (7), pp.671-690. <hal-01367066>
  • M. D'Ottavio, E. Carrera. Variable-kinematics approach for linearized buckling analysis of laminated plates and shells. AIAA Journal, American Institute of Aeronautics and Astronautics, 2010, 48 (9), pp.1987-1996. <hal-01367072>
  • M. D'Ottavio, O. Polit. Sensitivity analysis of thickness assumptions for piezoelectric plate models. Journal of Intelligent Material Systems and Structures, SAGE Publications (UK and US), 2009, 20 (15), pp.1815-1834. <hal-01367077>
  • T. Wallmersperger, F. K. Wittel, M. D'Ottavio, B. Kröplin. Multiscale Modeling of Polymer Gels ― Chemo-Electric Model versus Discrete Element Model. Mechanics of Advanced Materials and Structures, Taylor & Francis, 2008, 15 (3-4), pp.228-234. <hal-01367080>
  • M. D'Ottavio, B. Kröplin. Classical and Advanced Models for Laminated Plates with Piezoelectric Layers Actuated in Shear Mode. Mechanics of Advanced Materials and Structures, Taylor & Francis, 2008, 15 (3-4), pp.167 - 181. <hal-01367079>
  • M. D'Ottavio, B. Kröplin. An extension of Reissner Mixed Variational Theorem to piezoelectric laminates. Mechanics of Advanced Materials and Structures, Taylor & Francis, 2006, 13 (2), pp.139-150. <hal-01367089>
  • M. D'Ottavio, D. Ballhause, T. Wallmersperger, B. Kröplin. Considerations on higher-order finite elements for multilayered plates based on a unified formulation. Computers and Structures, Elsevier, 2006, 84 (19-20), pp.1222-1235. <hal-01367082>
  • M. D'Ottavio, D. Ballhause, B. Kröplin, E. Carrera. Closed-form solutions for the free-vibration problem of multilayered piezoelectric shells. Computers and Structures, Elsevier, 2006, 84 (22-23), pp.1506-1518. <hal-01367083>
  • K. Wolf, U. Scholl, P. Post, J.-V. Peetz, M. D'Ottavio, et al.. Verbesserung der Prognosefähigkeit der Crashsimulation aus höherfesten Merphasenstählen durch Berücksichtigung von Ergebnissen vorangestellter Umformsimulationen. FAT Schriftenreihe, 2005, 198. <hal-01367094>
  • D. Ballhause, M. D'Ottavio, B. Kröplin, E. Carrera. A unified formulation to assess multilayered theories for piezoelectric plates. Computers and Structures, Elsevier, 2005, 83 (15-16), pp.1217-1235. <hal-01367092>

Chapitre d'ouvrage6 documents

  • O. Polit, M. D'Ottavio, P. Vidal. Thermal Stress Analysis of Homogeneous and Laminated Shells by Finite Element Method. R. B. Hetnarski. Encyclopedia of Thermal Stresses, Springer Netherlands, 2014, 978-94-007-2740-3. <hal-01367043>
  • M. König, M. D'Ottavio. Models for Delamination. R.~Blockley and W.~Shyy. Encyclopedia of Aerospace Engineering, 13, John Wiley: Chichester, 2012, <10.1002/9780470686652.eae172.pub2>. <hal-01367064>
  • M. König, M. D'Ottavio. Models for Delamination. R. Blockley and W. Shyy. Encyclopedia of Aerospace Engineering, 13, John Wiley & Sons, Ltd., 2010, 9780470686652. <10.1002/9780470686652.eae172.pub2>. <hal-01367073>
  • M. D'Ottavio, F. K. Wittel, J. Reiser. Mechanism Based Toolbox: Prototypical Implementation of Tools. G. Busse and B. Kröplin and F.K. Wittel. Damage and its Evolution in Fiber-Composite Materials: Simulation and Non-Destructive Evaluation, ISD Verlag, pp.481-518, 2006, 3-930683-90-3. <hal-01367088>
  • M. D'Ottavio, M. König. Numerical Models for Delamination. G. Busse and B. Kröplin and F.K. Wittel. Damage and its Evolution in Fiber-Composite Materials: Simulation and Non-Destructive Evaluation, ISD Verlag, pp.381-424, 2006, 3-930683-90-3. <hal-01367086>
  • F. K. Wittel, M. D'Ottavio. An Open Toolbox for Damage Simulation. G. Busse and B. Kröplin and F.K. Wittel. Damage and its Evolution in Fiber-Composite Materials: Simulation and Non-Destructive Evaluation, ISD Verlag, pp.475-480, 2006, 3-930683-90-3. <hal-01367087>

Rapport5 documents

  • M. D'Ottavio, O. Polit, M. Kane. Digital mock-up of full-scale Anuloid aircraft. [Research Report] EU. 2014. <hal-01367048>
  • E. Carrera, G. Iuso, M. Petrolo, M. D'Ottavio, C. De Visser, et al.. First interim progress report. [Research Report] EU. 2014. <hal-01367049>
  • M. D'Ottavio, O. Polit, Z. Janda, M. Kane, J.-L. Bolteau. Fuselage with integrated power means, flight control means and other devices. [Research Report] EU. 2014. <hal-01367051>
  • E. Carrera, M. D'Ottavio, M. Petrolo, O. Polit. Comparison of Anuloid aircraft with other VTOL aircraft. [Research Report] EU. 2013. <hal-01367057>
  • E. Carrera, M. D'Ottavio, M. Petrolo, O. Polit. Initial configuration setup. [Research Report] EU. 2013. <hal-01367058>