- Abstract:
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This thesis presents a multidisciplinary and multi-objective design optimisation framework for transonic fan blades of modern high bypass ratio turbofan engines. The optimisation strategy applied is based on a twolevel approach consisting of a Differential Evolution algorithm coupled to a sequentially updated ordinary Kriging metamodel to accelerate the optimisation process. Aerodynamic as well as structural static and dynamic performance criteria are considered by means of high-fide...
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- Role:
- Supervisor
- Research group:
- von Karman Institute for Fluid Dynamics
- Role:
- Supervisor
- Type of award:
- DPhil
- Level of award:
- Doctoral
- Awarding institution:
- University of Oxford
- UUID:
-
uuid:2542beaf-2746-444d-8c3c-d1907d1e5d22
- Language:
- English
- Copyright holder:
- Chahine, C
- Copyright date:
- 2018
Thesis
Multidisciplinary design optimisation of aero-engine fan blades
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Authors
Contributors
+ He, L
+ Verstraete, T
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