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  - 2024/12/27

ER  -