Master's Dissertation
2004
A new sonic box formulation for oscillating swept thick wings in transonic flow.
Author
Guilherme Augusto Vargas Cesar
Advisor
- Advisor Paulo Afonso de Oliveira Soviero
Concentration Area
Aerodinâmica, Propulsão e Energia
Defense Date
2004
Thesis Number
000529639
Abstract
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.
Keywords
Aerodinâmica não-estacionária
Método dos painéis (dinâmica dos fluídos)
Escoamento transônico
Asas
Placas espessas
Modelos matemáticos
Física
Engenharia aeronáutica
