Optimal Design of a High-Altitude Solar-Powered Unmanned Airplane

Autor(es)

de Mattos, Bento Silva ; Secco, Ney Rafael ; Salles, Eduardo Francisco

• Tipo de documento: Artigo Científico
• Fonte: JOURNAL OF AEROSPACE TECHNOLOGY AND MANAGEMENT; v. 5, n. 3, p. 13-pg., 2013-07-01.

Resumo

This paper describes a multi-disciplinary design and optimization framework tailored for the conceptual development of high-altitude solar-powered unmanned aerial vehicles. The aircraft baseline configuration that the framework is able to handle is very similar to that of Zephyr, which is developed by the UK based company QinetiQ. The disciplines of aerodynamics, structures, stability, weight, and systems were considered and integrated into a modeFrontier (R) workflow, capable of providing a relatively simple sizing, but highly realistic airplane. (AU)

• Processo FAPESP: 07/00305-5 - Simulação numérica de alto desempenho aplicada à otimização de projeto de aeronave
• Beneficiário: Nide Geraldo do Couto Ramos Fico Júnior
• Modalidade de apoio: Auxílio à Pesquisa - Regular