TY - CONF T1 - Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings JO - 53rd AIAA Aerospace Sciences Meeting UR - http://eprints.whiterose.ac.uk/86371/ PY - 2015/01/05 AU - Zhu F AU - Qin N ED - DO - DOI: 10.2514/6.2015-1488 PB - American Institute of Aeronautics and Astronautics Y2 - 2025/04/09 ER -