This paper investigates the adequacy of radial basis function (RBF)-based models as surrogates in uncertainty quantification (UQ) and CFD shape optimization; for the latter, problems with and without uncertainties are considered. In UQ, these are used to support the Monte Carlo, as well as, the non-intrusive, Gauss Quadrature and regression-based polynomial chaos expansion methods. They are applied to the flow around an isolated airfoil and a wing to quantify uncertainties associated with the constants of the γ−R˜eθt transition model and the surface roughness (in the 3D case); it is demonstrated that the use of the RBF-based surrogates leads to an up to 50% reduction in computational cost, compared with the same UQ method that uses CFD comp...
We will present surrogate-based robust shape optimization of transonic airfoils. A large number of g...
This paper presents an effective approach for uncertain aerodynamic analysis of airfoils via the pol...
International audienceThis chapter describes the methodology used to construct Kriging-based surroga...
Uncertainty quantification (UQ) in aerodynamic simulations is retarded by the high computational cos...
Uncertainty quantification (UQ) in aerodynamic simulations is hindered by the high computational cos...
This chapter introduces the use of aerodynamic shape optimization applied to industrial problems, mo...
For many engineering problems, reliability and robustness are far more important than the nominal pe...
The objective of this paper was to introduce a computationally efficient approach for robust aerodyn...
For many engineering problems, reliability and robustness are far more important than the nominal pe...
The effort of quantifying the aerodynamic uncertainties caused by uncertainties in the airfoil geome...
Surrogate models are widely used as approximations to exact functions that are computationally expen...
When modeling physical systems, several sources of uncertainty are present. For example, variability...
Uncertainties, in the form of either non–predictable shape imperfections (manufacturing) or flow con...
Abstract Uncertainties, in the form of either non–predictable shape imperfections (manufacturing) or...
Uncertainty analysis is of great use both for calculating outputs that are more akin to real flight,...
We will present surrogate-based robust shape optimization of transonic airfoils. A large number of g...
This paper presents an effective approach for uncertain aerodynamic analysis of airfoils via the pol...
International audienceThis chapter describes the methodology used to construct Kriging-based surroga...
Uncertainty quantification (UQ) in aerodynamic simulations is retarded by the high computational cos...
Uncertainty quantification (UQ) in aerodynamic simulations is hindered by the high computational cos...
This chapter introduces the use of aerodynamic shape optimization applied to industrial problems, mo...
For many engineering problems, reliability and robustness are far more important than the nominal pe...
The objective of this paper was to introduce a computationally efficient approach for robust aerodyn...
For many engineering problems, reliability and robustness are far more important than the nominal pe...
The effort of quantifying the aerodynamic uncertainties caused by uncertainties in the airfoil geome...
Surrogate models are widely used as approximations to exact functions that are computationally expen...
When modeling physical systems, several sources of uncertainty are present. For example, variability...
Uncertainties, in the form of either non–predictable shape imperfections (manufacturing) or flow con...
Abstract Uncertainties, in the form of either non–predictable shape imperfections (manufacturing) or...
Uncertainty analysis is of great use both for calculating outputs that are more akin to real flight,...
We will present surrogate-based robust shape optimization of transonic airfoils. A large number of g...
This paper presents an effective approach for uncertain aerodynamic analysis of airfoils via the pol...
International audienceThis chapter describes the methodology used to construct Kriging-based surroga...