A method of dynamic mesh based airfoil optimization is proposed according to the drawbacks of surrogate model based airfoil optimization. Programs are designed to achieve the dynamic mesh. Boundary condition is add by integrating commercial software Pointwise, meanwhile the CFD calculation is carried out by commercial software Fluent. The data exchange and communication between the software and programs referred above have been accomplished, and the whole optimization process is performed in iSIGHT platform. A simplified airfoil optimization study case is brought out to show that aerodynamic performances of airfoil have been significantly improved, even save massive repeat operations and increase the robustness and credibility of the optimi...
Surrogate-based optimization and efficient global optimization in particular, is considered fo...
Aerodynamic shape optimization of airfoils is carried out for two values of Reynolds numbers: 10<SUP...
The method of optimization algorithms is one of the most important parameters which will strongly in...
The all–at–once approach is implemented to solve an optimum airfoil design problem. The airfoil desi...
In this thesis, an airfoil design optimization with Computational Fluid Dynamics (CFD) analysis comb...
AbstractComputational fluid dynamics (CFD) is one of the computer-based solution methods which is mo...
Practical aerodynamic design problems must balance the goal of performance optimization over a range...
An airfoil design technique is described which uses an analytical method for representing the airfoi...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140448/1/6.2014-2996.pd
Practical aerodynamic shape design problems must balance performance optimization over a range of on...
This paper demonstrates the big influence of the control of the mesh quality in the final solution o...
Adaptive mesh refinement is one of the most important tools in Computational Fluid Dynamics (CFD) fo...
The combination of the optimization software, modeFRONTIER and the commercial CFD software is used t...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
A design optimization technique is presented which couples a computationally efficient Navier-Stokes...
Surrogate-based optimization and efficient global optimization in particular, is considered fo...
Aerodynamic shape optimization of airfoils is carried out for two values of Reynolds numbers: 10<SUP...
The method of optimization algorithms is one of the most important parameters which will strongly in...
The all–at–once approach is implemented to solve an optimum airfoil design problem. The airfoil desi...
In this thesis, an airfoil design optimization with Computational Fluid Dynamics (CFD) analysis comb...
AbstractComputational fluid dynamics (CFD) is one of the computer-based solution methods which is mo...
Practical aerodynamic design problems must balance the goal of performance optimization over a range...
An airfoil design technique is described which uses an analytical method for representing the airfoi...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140448/1/6.2014-2996.pd
Practical aerodynamic shape design problems must balance performance optimization over a range of on...
This paper demonstrates the big influence of the control of the mesh quality in the final solution o...
Adaptive mesh refinement is one of the most important tools in Computational Fluid Dynamics (CFD) fo...
The combination of the optimization software, modeFRONTIER and the commercial CFD software is used t...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
A design optimization technique is presented which couples a computationally efficient Navier-Stokes...
Surrogate-based optimization and efficient global optimization in particular, is considered fo...
Aerodynamic shape optimization of airfoils is carried out for two values of Reynolds numbers: 10<SUP...
The method of optimization algorithms is one of the most important parameters which will strongly in...