TY  - CONF

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

JO  - ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition

UR  - https://eprints.whiterose.ac.uk/id/eprint/142876

PY  - 2018/06/30

AU  - John A

AU  - Qin N

AU  - Shahpar S

ED  - 

DO  - DOI: 10.1115/GT2018-77065

PB  - American Society of Mechanical Engineers

SN  - 978-0-7918-5099-2

VL  - 2A

Y2  - 2024/12/22

ER  -