Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear (2018)
- Authors:
- USP affiliated authors: CATALANO, FERNANDO MARTINI - EESC ; REGO, LEANDRO FALCÃO LOUREIRO - EESC ; PEREIRA, LOURENÇO TÉRCIO LIMA - EESC
- Unidade: EESC
- DOI: 10.2514/6.2018-0759
- Subjects: TRENS DE POUSO; ENGENHARIA AERONÁUTICA; AERODINÂMICA DE AERONAVES; AEROACÚSTICA
- Language: Inglês
- Imprenta:
- Publisher: AIAA
- Publisher place: Reston, VA, USA
- Date published: 2018
- Source:
- Título: Proceedings
- Conference titles: AAIA Aerospace Sciences Meeting
- Este periódico é de acesso aberto
- Este artigo NÃO é de acesso aberto
-
ABNT
REGO, Leandro Falcão Loureiro et al. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0759. Acesso em: 25 fev. 2026. -
APA
Rego, L. F. L., Pereira, L. T. L., Catalano, F. M., Speth, R., Bent, P., & Fregnani, J. A. (2018). Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-0759 -
NLM
Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2026 fev. 25 ] Available from: https://doi.org/10.2514/6.2018-0759 -
Vancouver
Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2026 fev. 25 ] Available from: https://doi.org/10.2514/6.2018-0759 - Noise reductions on a pusher propeller configuration through pylon tangential blowing
- Experimental slat noise assessment through phased array and hot-film anemometry measurements
- Evaluation of wind tunnel wall boundarylayer control for 2-D high-lift aerodynamic and aeroacoustic testing
- A study on the 3D effects of slat cove fillers
- Experimental and numerical analysis of the effect of "coanda" tip jets on the wing tip vortex
- Development of a pylon blowing system for a pusher propeller configuration with the study of the associated aerodynamic and aeroacustic phenomena
- Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model
- Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model
- Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model
- Parametric analysis of the influence of slat geometry on acoustic noise
Informações sobre o DOI: 10.2514/6.2018-0759 (Fonte: oaDOI API)
Download do texto completo
| Tipo | Nome | Link | |
|---|---|---|---|
 |
trabalho 11 - Aerodynamic... |
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
