Aircraft structures using composite materials

• Grant number: 06/61257-5
• Support Opportunities: Research Grants - Research Partnership for Technological Innovation - PITE
• Start date: May 01, 2011
• End date: April 30, 2015
• Field of knowledge: Engineering - Aerospace Engineering - Aerospace Structures
• Agreement: 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
• Company: Empresa Brasileira Aeronáutica S/A (EMBRAER)
• City: São José dos Campos

Scientific publications

(References retrieved automatically from Web of Science and SciELO through information on FAPESP grants and their corresponding numbers as mentioned in the publications by the authors)

DUTRA, THIAGO ASSIS; MUELLER DE ALMEIDA, SERGIO FRASCINO. Composite plate stiffness multicriteria optimization using lamination parameters. COMPOSITE STRUCTURES, v. 133, p. 166-177, DEC 1 2015. (08/57866-1, 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, FEB 2015. (12/18365-2, 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, MAY 2017. (06/61257-5)