Influence of sub boundary layer vortex generator height and attack angle on cross-flows in the hub region of compressors

Subjects

Subjects :

Physics
Boundary layer
Mechanical Engineering
Aerospace Engineering
Mechanics
Vortex generator
Gas compressor

Details

ISSN :

10009361

Volume :

35

Database :

OpenAIRE

Journal :

Chinese Journal of Aeronautics

Accession number :

edsair.doi...........5dce9965fa650a0bb86f4e6692969db0

Full Text :

https://doi.org/10.1016/j.cja.2021.11.013