TY  - CONF

T1  - Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings

JO  - 53rd AIAA Aerospace Sciences Meeting

UR  - https://eprints.whiterose.ac.uk/id/eprint/86371

UR  - https://doi.org/10.2514/6.2015-1488

PY  - 2015/01/05

AU  - Zhu F

AU  - Hinchliffe B

AU  - Qin N

ED  - 

DO  - DOI: 10.2514/6.2015-1488

PB  - American Institute of Aeronautics and Astronautics (AIAA)

SN  - 978-1-62410-343-8

IS  - 1488

Y2  - 2025/11/03

ER  -