Modal and non-modal instability analysis of low-Re 3D flow over NACA airfoils near and beyond stall (2015)
- Autores:
- Autor USP: GIORIA, RAFAEL DOS SANTOS - EP
- Unidade: EP
- Assunto: AERODINÂMICA
- Idioma: Inglês
- Imprenta:
- Nome do evento: Symposium on global flow instability and control
-
ABNT
HE, We et al. Modal and non-modal instability analysis of low-Re 3D flow over NACA airfoils near and beyond stall. 2015, Anais.. Crete: Escola Politécnica, Universidade de São Paulo, 2015. . Acesso em: 25 abr. 2024. -
APA
He, W., Gioria, R. dos S., Pérez, J. M., & Theofilis, V. (2015). Modal and non-modal instability analysis of low-Re 3D flow over NACA airfoils near and beyond stall. In . Crete: Escola Politécnica, Universidade de São Paulo. -
NLM
He W, Gioria R dos S, Pérez JM, Theofilis V. Modal and non-modal instability analysis of low-Re 3D flow over NACA airfoils near and beyond stall. 2015 ;[citado 2024 abr. 25 ] -
Vancouver
He W, Gioria R dos S, Pérez JM, Theofilis V. Modal and non-modal instability analysis of low-Re 3D flow over NACA airfoils near and beyond stall. 2015 ;[citado 2024 abr. 25 ] - Estudo da estabilidade secundária da esteira de um cilindro em oscilação forçada
- Linear instability of low Reynolds number massively separated flow around three NACA airfoils
- Modal and non-modal global instability analyses of low-Re massively separated flow around a NACA 0015 airfoil
- Sensibilidade a perturbações na condição de entrada em escoamentos internos
- On global linear instability mechanisms of flow around airfoils at low Reynolds number and high angle of attack
- SeismicMesh: triangular meshing for seismology
- Variable-width aerodynamic device
- Hybrid Machine Learning for Modeling the Relative Permeability Changes in Carbonate Reservoirs under Engineered Water Injection
- Variable-width aerodynamic device for reducing aerodynamically generated noise in aerodynamic high lift structure e.g. flap, has longitudinal edge and non-rectilinear longitudinal edge that defines variable width along length
- Optimization of liquid jet ejector geometry and its impact on flow fields
Como citar
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
