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 - 2025/05/19 ER -