TY  - CONF

T1  - Using Shock Control Bumps to Improve Transonic Fan/Compressor Blade Performance

JO  - Volume 2A: Turbomachinery

UR  - http://eprints.whiterose.ac.uk/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  - 9780791850992

Y2  - 2024/12/22

ER  -