Gas–liquid flow field analysis of the compressor vorticity and rotational speed based on NASA Stage 36

Gas–liquid flow field analysis of the compressor vorticity and rotational speed based on NASA Stage 36

The aero-engine to be cleaned online can significantly improve compressor performance and increase maintenance intervals, but the cleaning online cannot achieve the anticipated effects due to the lack of cognisance of the internal multiphase flow field. In order to explore the characteristics of the...

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Détails bibliographiques
Auteurs principaux: Liwen Wang, Jianwei Hu, Qiang Liu, Jie Tang, Xudong Shi
Format: Article
Langue:English
Publié: Wiley 2018-11-01
Collection:The Journal of Engineering
Sujets:
compressors
two-phase flow
aerospace engines
nozzles
blades
computational fluid dynamics
vortices
flow simulation
channel flow
jets
gas–liquid flow field analysis
compressor vorticity
rotational speed
internal multiphase flow field
Rotor36 compressor blades
fluid simulation software
circumferential vortex
axial vortex
aeroengine
jet parameters
NASA Stage 36
nozzle flow channel
pressure 5.0 atm
Accès en ligne:https://digital-library.theiet.org/content/journals/10.1049/joe.2018.9019

Internet

https://digital-library.theiet.org/content/journals/10.1049/joe.2018.9019

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