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Aircraft structures using composite materials

Grant number: 06/61257-5
Support Opportunities:Research Grants - Research Partnership for Technological Innovation - PITE
Duration: May 01, 2011 - April 30, 2015
Field of knowledge:Engineering - Aerospace Engineering - Aerospace Structures
Convênio/Acordo: Embraer
Principal Investigator:Sergio Frascino Muller de Almeida
Grantee:Sergio Frascino Muller de Almeida
Host Institution: Divisão de Engenharia Mecânica (IEM). Instituto Tecnológico de Aeronáutica (ITA). Ministério da Defesa (Brasil). São José dos Campos , SP, Brazil
Host Company: Empresa Brasileira Aeronáutica S/A (EMBRAER)
City: São José dos Campos
Articles published in Agência FAPESP Newsletter about the research grant:
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Articles published in other media outlets ( ):
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VEICULO: TITULO (DATA)
VEICULO: TITULO (DATA)

Publicações científicas
(Referências obtidas automaticamente do Web of Science e do SciELO, por meio da informação sobre o financiamento pela FAPESP e o número do processo correspondente, incluída na publicação pelos autores)
DUTRA, THIAGO ASSIS; MUELLER DE ALMEIDA, SERGIO FRASCINO. Composite plate stiffness multicriteria optimization using lamination parameters. COMPOSITE STRUCTURES, v. 133, p. 166-177, . (08/57866-1, 06/61257-5)
MENDONCA SALES, RITA DE CASSIA; GUSMAO, SILAS RODRIGO; GOUVEA, RICARDO FRANCISCO; CHU, THOMAS; FERNANDEZ MARLET, JOSE MARIA; CANDIDO, GERALDO MAURICIO; DONADON, MAURICIO VICENTE. The temperature effects on the fracture toughness of carbon fiber/RTM-6 laminates processed by VARTM. JOURNAL OF COMPOSITE MATERIALS, v. 51, n. 12, p. 1729-1741, . (06/61257-5)
GEHLEN ROHRER, RUBENS ZOLAR; MULLER DE ALMEIDA, SERGIO FRASCINO; DONADON, MAURICIO VICENTE. Optimization of composite plates subjected to buckling and small mass impact using lamination parameters. COMPOSITE STRUCTURES, v. 120, p. 141-152, . (12/18365-2, 08/57866-1, 06/61257-5)

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