Effect of fan root flow on the low-pressure compressor transition duct for an ultra high bypass ratio turbofan engine

Subjects

Subjects :

s-duct
compressor transition duct
Secondary flow
cfd model
five-hole probes
Hotwire
Phase-locked measurements
Aerodynamics
turbomachinery
Rotor-design
Turbofan Engines

Details

Language :

English

Database :

British Library EThOS

Publication Type :

Dissertation/ Thesis

Accession number :

edsble.878672

Document Type :

Electronic Thesis or Dissertation

Full Text :

https://doi.org/10.26174/thesis.lboro.22596061.v1