In order to improve product characteristics, engineering design makes increasing use of Robust Design and Multidisciplinary Design Optimisation. Common to both methodologies is the need to vary the object’s shape and to assess the resulting change in performance, both executed within an automatic loop. This shape change can be realised by modifying the parameter values of a suitably parameterised Computer Aided Design (CAD) model. This paper presents the adopted methodology and the achieved results when performing optimisation of a gas turbine disk. Our approach to hierarchical modelling employing design tables is presented, with methods to ensure satisfactory geometry variation by commercial CAD systems. The conducted studies included stoc...
The present thesis incorporates the CAD model into an adjoint-based optimization loop and uses it fo...
The adjoint method is considered as the most efficient approach to compute gradients with respect to...
Turbine blade life is central to the integrity of the aircraft engine. Manufacturing variability may...
The effective application of various optimisation techniques including classic gradient-based and mo...
This paper addresses the problem of turbine blade shape optimization in the presence of geometric un...
This paper is concerned with automation and optimisation of the design of a turbine blade fir-tree r...
The main goal in jet engine design is to achieve light, compact and highly efficient systems while r...
The objective of this research is to develop a methodology for incorporating cost models based on ma...
Automatic design methods are changing the approach to and processes involved in gas turbine design. ...
The use of CFD-based optimizations is becoming a standard for turbomachinery design. Although the us...
This paper describes the project GivEn that develops a novel multicriteria optimization process for ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.In...
The gas turbine engine has evolved rapidly during past decades to provide a reliable and efficient b...
Nowadays, product configuration and optimization are very important topics in several industrial app...
The so-called Green Engine architectures are deeply investigated by the scientific community with th...
The present thesis incorporates the CAD model into an adjoint-based optimization loop and uses it fo...
The adjoint method is considered as the most efficient approach to compute gradients with respect to...
Turbine blade life is central to the integrity of the aircraft engine. Manufacturing variability may...
The effective application of various optimisation techniques including classic gradient-based and mo...
This paper addresses the problem of turbine blade shape optimization in the presence of geometric un...
This paper is concerned with automation and optimisation of the design of a turbine blade fir-tree r...
The main goal in jet engine design is to achieve light, compact and highly efficient systems while r...
The objective of this research is to develop a methodology for incorporating cost models based on ma...
Automatic design methods are changing the approach to and processes involved in gas turbine design. ...
The use of CFD-based optimizations is becoming a standard for turbomachinery design. Although the us...
This paper describes the project GivEn that develops a novel multicriteria optimization process for ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.In...
The gas turbine engine has evolved rapidly during past decades to provide a reliable and efficient b...
Nowadays, product configuration and optimization are very important topics in several industrial app...
The so-called Green Engine architectures are deeply investigated by the scientific community with th...
The present thesis incorporates the CAD model into an adjoint-based optimization loop and uses it fo...
The adjoint method is considered as the most efficient approach to compute gradients with respect to...
Turbine blade life is central to the integrity of the aircraft engine. Manufacturing variability may...