TY  - JOUR

T1  - Using shock control bumps to improve transonic fan/compressor blade performance

JO  - Journal of Turbomachinery

UR  - https://eprints.whiterose.ac.uk/id/eprint/142878

PY  - 2019/08/01

AU  - John A

AU  - Qin N

AU  - Shahpar S

ED  - 

DO  - DOI: 10.1115/1.4042891

PB  - ASME

VL  - 141

IS  - 8

Y2  - 2025/04/27

ER  -