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 - 2025/05/31 ER -