Dissertação de Mestrado
2004
A new sonic box formulation for oscillating swept thick wings in transonic flow.
Autor
Guilherme Augusto Vargas Cesar
Orientador
- Orientador Paulo Afonso de Oliveira Soviero
Área de Concentração
Aerodinâmica, Propulsão e Energia
Data de Defesa
2004
Número da Tese
000529639
Resumo
The present work shows a mathematical model for unsteady linearized potential flow around thin wings having swept leading and trailing edges and over thick wings with swept and unswept leading edges. Doublet integrals are obtained for the three dimensional case. The wings are supposed to be describing small amplitude harmonic motions of pitch and plunge. Exact solutions for thin and thick wings oscillating on an unsteady potential sonic flow are presented and are compared with other works.
Palavras-chave
Aerodinâmica não-estacionária
Método dos painéis (dinâmica dos fluídos)
Escoamento transônico
Asas
Placas espessas
Modelos matemáticos
Física
Engenharia aeronáutica
