The research presented treats the robust design optimization (RDO) of an unmanned aerialvehicle (UAV) considering geometric uncertainty related to its production process. RDO re-quires uncertainty quantification (UQ) in a number of design points, making it computationallyexpensive. Therefore, surrogate modelling is employed to efficiently perform the optimization.The optimization is regarded as a multi-objective optimization (MOO) of expected value andvariance. The goal is to obtain a Pareto set of non-dominated solutions. Several methods areassessed by applying them to an analytical test function. Subsequently, the RDO of a UAV with forward swept planform and the validation of the resulting optimal points are performed
An alternative methodology that views aircraft configuration development from an optimization perspe...
In order to be able to assess also unconventional aircraft configurations, aircraft designers need t...
We will present surrogate-based robust shape optimization of transonic airfoils. A large number of g...
The research presented treats the robust design optimization (RDO) of an unmanned aerialvehicle (UAV...
In this paper the design optimization-under-uncertainty of a forward swept wing (FSW) blended wing b...
When designing an aircraft engineers are usually given a design or set of design points especially o...
In this work, robust design optimization (RDO) is treated, motivated by the increasing desire to acc...
There are many applications in aeronautical/aerospace engineering where some values of the design pa...
This paper deals with developing an efficient Robust Design Optimization (RDO) framework. The goal i...
openVirtual design analysis has become an indispensable component in most engineering disciplines. D...
This chapter introduces the use of aerodynamic shape optimization applied to industrial problems, mo...
In this paper, the multi-objective, multifidelity optimization of a wing fence on an unmanned aerial...
This paper examines robust optimization design and analysis of a conformal expansion nozzle of flyin...
Efficient surrogate modeling approaches are presented in the context of robust design. The type of s...
The assessment of uncertainties is essential in aerodynamic shape optimization problems to come up w...
An alternative methodology that views aircraft configuration development from an optimization perspe...
In order to be able to assess also unconventional aircraft configurations, aircraft designers need t...
We will present surrogate-based robust shape optimization of transonic airfoils. A large number of g...
The research presented treats the robust design optimization (RDO) of an unmanned aerialvehicle (UAV...
In this paper the design optimization-under-uncertainty of a forward swept wing (FSW) blended wing b...
When designing an aircraft engineers are usually given a design or set of design points especially o...
In this work, robust design optimization (RDO) is treated, motivated by the increasing desire to acc...
There are many applications in aeronautical/aerospace engineering where some values of the design pa...
This paper deals with developing an efficient Robust Design Optimization (RDO) framework. The goal i...
openVirtual design analysis has become an indispensable component in most engineering disciplines. D...
This chapter introduces the use of aerodynamic shape optimization applied to industrial problems, mo...
In this paper, the multi-objective, multifidelity optimization of a wing fence on an unmanned aerial...
This paper examines robust optimization design and analysis of a conformal expansion nozzle of flyin...
Efficient surrogate modeling approaches are presented in the context of robust design. The type of s...
The assessment of uncertainties is essential in aerodynamic shape optimization problems to come up w...
An alternative methodology that views aircraft configuration development from an optimization perspe...
In order to be able to assess also unconventional aircraft configurations, aircraft designers need t...
We will present surrogate-based robust shape optimization of transonic airfoils. A large number of g...