Natural Laminar Flow Wing Design and Optimisation
Supervisors: Professor N Qin, Dr R Howell
This study will investigate the design and optimisation of NLF wings for transonic flow. The stability of the boundary layer around the wing including cross flow instability and attachment line instability will be studied. The wing will be optimised for minimum drag.
Previous experience / requirements: Aerodynamics / CFD
n.qin@sheffield.ac.uk
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