This work presents a framework for the optimisation of certain aspects of a BERP-like (British Experimental Rotor Programme) rotor blade in hover and forward flight so that maximum performance can be obtained from the blade. The proposed method employs a high-fidelity, efficient CFD technique that uses the Harmonic Balance method in conjunction with artificial neural networks (ANNs) as metamodels, and genetic algorithms (GAs) for optimisation. The approach has been previously demonstrated for the optimisation of blade twist in hover and the optimisation of rotor sections in forward flight, transonic aerofoils design, wing and rotor tip planforms. In this paper, a parameterisation technique was devised for the BERP-like rotor tip and its par...
This paper presents a description of the method and results of rotor blade shape optimization. The r...
The increased need to design higher performing aerodynamic shapes has led to design optimisation cyc...
A short overview of the main techniques for turbomachinery blade design based on CFD is followed by ...
This work presents a framework for the optimization of certain aspects of a British Experimental Rot...
This chapter describes the optimisation of a BERP-like rotor planform using an optimisation method t...
This work presents a framework for the optimisation of various aspects of rotor blades in forward fl...
This work presents a method for the optimisation of aspects of rotor blade shape in forward flight. ...
This work presents a computational framework for the optimisation of various aspects of rotor blades...
This work aims to develop a framework for the optimisation of various aspects of rotor blades. The p...
Abstract-A new approach to high-fidelity aerodynamic design optimization of a wind turbine blade con...
Industrial aerodynamic design optimization of helicopter rotor blades requires employ-ment of multi-...
This study presents a methodology first built up for the aerodynamic shape optimization for wind tur...
This study aims to determine optimal locations of dual trailing-edge flaps and blade stiffness to ac...
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. The Aerod...
A variety of methods have been developed, and the majority of the applications have been for cases t...
This paper presents a description of the method and results of rotor blade shape optimization. The r...
The increased need to design higher performing aerodynamic shapes has led to design optimisation cyc...
A short overview of the main techniques for turbomachinery blade design based on CFD is followed by ...
This work presents a framework for the optimization of certain aspects of a British Experimental Rot...
This chapter describes the optimisation of a BERP-like rotor planform using an optimisation method t...
This work presents a framework for the optimisation of various aspects of rotor blades in forward fl...
This work presents a method for the optimisation of aspects of rotor blade shape in forward flight. ...
This work presents a computational framework for the optimisation of various aspects of rotor blades...
This work aims to develop a framework for the optimisation of various aspects of rotor blades. The p...
Abstract-A new approach to high-fidelity aerodynamic design optimization of a wind turbine blade con...
Industrial aerodynamic design optimization of helicopter rotor blades requires employ-ment of multi-...
This study presents a methodology first built up for the aerodynamic shape optimization for wind tur...
This study aims to determine optimal locations of dual trailing-edge flaps and blade stiffness to ac...
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. The Aerod...
A variety of methods have been developed, and the majority of the applications have been for cases t...
This paper presents a description of the method and results of rotor blade shape optimization. The r...
The increased need to design higher performing aerodynamic shapes has led to design optimisation cyc...
A short overview of the main techniques for turbomachinery blade design based on CFD is followed by ...