TY - JOUR
T1 - Using shock control bumps to improve transonic fan/compressor blade performance
JO - Journal of Turbomachinery
UR - http://eprints.whiterose.ac.uk/142878/
PY - 2019/08/01
AU - John A
AU - Qin N
AU - Shahpar S
ED -
DO - DOI: 10.1115/1.4042891
VL - 141
IS - 8
Y2 - 2025/01/02
ER -