This viewgraph presentation gives an overview of global optimization techniques for fluid flow and propulsion devices. Details are given on the need, characteristics, and techniques for global optimization. The techniques include response surface methodology (RSM), neural networks and back-propagation neural networks, design of experiments, face centered composite design (FCCD), orthogonal arrays, outlier analysis, and design optimization
The grant closure report is organized in the following four chapters: Chapter describes the two rese...
Abstract:- This article addresses the issue of selecting surrogate models suitable for the global op...
The increased need to design higher performing aerodynamic shapes has led to design optimisation cyc...
Modern computational and experimental tools for aerodynamics and propulsion applications have mature...
Modern computational and experimental tools for aerodynamics and propulsion applications have mature...
Drawing on extensive research and experience, this timely reference brings together numerical optimi...
An optimization methodology based on neural networks was developed for use in 2D optimal shape desig...
This paper describes the combination of several optimization technologies that can be used to tackle...
Turbine performance directly affects engine specific impulse, thrust-to-weight ratio, and cost in a ...
The increased need to design higher performing aerodynamic shapes has led to design optimization cyc...
The increased need to design higher performing aerodynamic shapes has led to design optimization cyc...
There is growing interest to adopt supersonic turbines for rocket propulsion. However, this technolo...
The research conducted and resumed in this thesis covers two different topics. In chapter 1, I f...
Although generally speaking, a great number of functional evaluations may be required until converge...
General problems of interest in computational fluid dynamics are investigated by means of optimizati...
The grant closure report is organized in the following four chapters: Chapter describes the two rese...
Abstract:- This article addresses the issue of selecting surrogate models suitable for the global op...
The increased need to design higher performing aerodynamic shapes has led to design optimisation cyc...
Modern computational and experimental tools for aerodynamics and propulsion applications have mature...
Modern computational and experimental tools for aerodynamics and propulsion applications have mature...
Drawing on extensive research and experience, this timely reference brings together numerical optimi...
An optimization methodology based on neural networks was developed for use in 2D optimal shape desig...
This paper describes the combination of several optimization technologies that can be used to tackle...
Turbine performance directly affects engine specific impulse, thrust-to-weight ratio, and cost in a ...
The increased need to design higher performing aerodynamic shapes has led to design optimization cyc...
The increased need to design higher performing aerodynamic shapes has led to design optimization cyc...
There is growing interest to adopt supersonic turbines for rocket propulsion. However, this technolo...
The research conducted and resumed in this thesis covers two different topics. In chapter 1, I f...
Although generally speaking, a great number of functional evaluations may be required until converge...
General problems of interest in computational fluid dynamics are investigated by means of optimizati...
The grant closure report is organized in the following four chapters: Chapter describes the two rese...
Abstract:- This article addresses the issue of selecting surrogate models suitable for the global op...
The increased need to design higher performing aerodynamic shapes has led to design optimisation cyc...