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pro vyhledávání: '"Alberto Baretter"'
Autor:
Alberto Baretter, Benjamin Godard, Pierric Joseph, Olivier Roussette, Francesco Romanò, Raphael Barrier, Antoine Dazin
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power, Vol 6, Iss 4, p 43 (2021)
On many occasions, fan or compressor stages have to face azimuthal flow distortion at inlet, which affects their performance and stability. These flow distortions can be caused by external events or by some particular geometrical features. The aim of
Externí odkaz:
https://doaj.org/article/6df6a38644404c7eafec0a259d0f7e82
Publikováno v:
Volume 10A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics.
In aircraft engines, compressor stages can encounter situations in which the flow is distorted at rotor inlet, for example during particular flight maneuvers, or due to the shape of the inlet of the airframe. The main objective of this paper is to in
Autor:
Francesco Romanò, Benjamin Godard, Antoine Dazin, Alberto Baretter, Olivier Roussette, Pierric Joseph, Raphaël Barrier
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power
International Journal of Turbomachinery, Propulsion and Power, 2021, 6 (4), pp.43. ⟨10.3390/ijtpp6040043⟩
International Journal of Turbomachinery, Propulsion and Power, Vol 6, Iss 43, p 43 (2021)
International Journal of Turbomachinery, Propulsion and Power; Volume 6; Issue 4; Pages: 43
International Journal of Turbomachinery, Propulsion and Power, 2021, 6 (4), pp.43. ⟨10.3390/ijtpp6040043⟩
International Journal of Turbomachinery, Propulsion and Power, Vol 6, Iss 43, p 43 (2021)
International Journal of Turbomachinery, Propulsion and Power; Volume 6; Issue 4; Pages: 43
The aeronautical industry is facing stronger and stronger challenges to respect the legal constraint concerning the CO2 and pollutant emissions. To address these challenges, the well-known Boundary Layer Ingestion (BLI) method certainly holds a lot o
Publikováno v:
European Conference on Turbomachinery Fluid Dynamics and hermodynamics.
The Channel Tunnel is made up of 2 long railway tunnels of about 50 km long and connected every 250 m by 2 m diameter pipes. These pipes, called piston relief ducts, allow the air pushed by a train to go from one tunnel to another to limit the piston