CV Lattes
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Ministério da Defesa (Brasil). Instituto Tecnológico de Aeronáutica (ITA). Divisão de Engenharia Mecânica (IEM) (Institutional affiliation from the last research proposal) Birthplace: Brazil
He holds an undergratuate degree in Mechanical Engineering from Instituto Tecnológico de Aeronáutica (1978), master degree in Aerospace Engineering from Instituto Tecnológico de Aeronáutica (1982) and Ph.D. in Aerospace Engineering from University of Kansas (1986). He has expertise in Composite Materials Aerospace Structures acting on the following subjects: composite materials, finite elements, buckling, vibrations and design.Currently he is a Professor at the Mechanical Departament of Faculty of Engineering of Guaratinguetá / State University of São Paulo. (Source: Lattes Curriculum)
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The "offshore of tomorrow" is being defined in our generation. Awaken by climate change, we were made aware that the exploration of fossil fuels for the sole use of thermal energy cannot be sustainable in the distant future. The effect humanity has played in changing the climate of the planet by the emission of greenhouse gases is a pressing agenda for many, if not all, countries committe…
The FAPESP - Shell Research Centre for Greenhouse Gas Innovation aims to be a world-class Centre for advanced studies with a focus on innovation towards sustainability and mitigation of greenhouse gas emissions. The Centre complements Fapesp's experiences in supporting high-level scientific research and technology development towards these fields. It aims to establish a world-class Centre…
This document presents a research proposal with the objective of obtaining financial support for a technical visit of Professor Jorn S. Hansen, from the University of Toronto; Institute for Aerospace Studies (UTIAS) to the Instituto Tecnológico de Aeronáutica (ITA). The research deals with the buckling and post-buckling of stiffened composite panels and shells, which are of direct relevan…
(Only some records are available in English at this moment)
The present project aim to develop optimization innovative techniques applied to aeronautical panels manufactured in composite material under simultaneous action of compressive and impact of small mass loads.The objective function is the maximization of the bending load of a panel with a certain number of plies under eventual degradation effects caused by impact loads. The project variabl…
This work deals with the numerical and experimental investigation of the structural behavior of laminated composite panels subjected to in-plane shear loads.The objective is to develop a test device for laminated panels subjected to shear loads, experimentally characterize the out of plane displacement field in post-buckling using non-contact optical devices (topogrammetry) and correlate …
| 2 / 2 | Ongoing grants |
| 8 / 4 | Completed research grants |
| 10 / 3 | Completed scholarships in Brazil |
| 1 / 0 | Completed scholarships abroad |
| 21 / 9 | All research grants and scholarships |
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