@article{article, title  = {{Using shock control bumps to improve transonic fan/compressor blade performance}},

 publisher = {{ASME}},

 url = {{https://eprints.whiterose.ac.uk/id/eprint/142878 }},

 year = {{2019}},

 month = {{8}},

 author = {{John A and Qin N and Shahpar S}},

 doi = {{10.1115/1.4042891}},

 volume = {{141}},

 journal = {{Journal of Turbomachinery}},

 issue = {{8}},

 note = {{Accessed on 2024/12/22}}}