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[[File:GEK airfoil reference.png|thumb|400px|Reference results for the drag coefficient of a transonic airfoil, based on a large number of CFD simulations. The horizontal and vertical axis show the deformation of the shape of the airfoil.]]
[[File:GEK airfoil reference.png|thumb|400px|Reference results for the drag coefficient of a transonic airfoil, based on a large number of CFD simulations. The horizontal and vertical axis show the deformation of the shape of the airfoil.]]


[[File:GEK airfoil Kriging.png|thumb|400px|Kriging surrogate model of the drag coefficient of a transonic airfoil.]]
[[File:GEK airfoil Kriging.png|thumb|400px|Kriging surrogate model of the drag coefficient of a transonic airfoil. The gray dots indicate the configurations for which the CFD solver was run.]]


[[File:GEK airfoil GEK.png|thumb|400px|GEK surrogate model of the drag coefficient of a transonic airfoil.]]
[[File:GEK airfoil GEK.png|thumb|400px|GEK surrogate model of the drag coefficient of a transonic airfoil. The gray dots indicate the configurations for which the CFD solver was run, the arrows indicate the gradients.]]


== References ==
== References ==

Revision as of 03:26, 8 November 2016

Template:New unreviewed article Gradient-Enhanced Kriging (GEK) is a surrogate modeling technique used in engineering. A surrogate model (alternatively known as a metamodel, response surface or emulator) is a prediction of the output of an expensive computer code. This prediction is based on a small number of evaluations of the expensive computer code.

Introduction

Example of one-dimensional data interpolated by Kriging and GEK. The black line indicates the test-function, while the gray circles indicate 'samples' or evaluations of the test-function. The blue line is the Kriging mean, the shaded blue area illustrates the Kriging standard deviation. With GEK we can add the gradient information, illustrated in red, which increases the accuracy of the prediction.

Predictor equations

Kriging

GEK

Example: Drag coefficient of a transonic airfoil

Reference results for the drag coefficient of a transonic airfoil, based on a large number of CFD simulations. The horizontal and vertical axis show the deformation of the shape of the airfoil.
Kriging surrogate model of the drag coefficient of a transonic airfoil. The gray dots indicate the configurations for which the CFD solver was run.
GEK surrogate model of the drag coefficient of a transonic airfoil. The gray dots indicate the configurations for which the CFD solver was run, the arrows indicate the gradients.

References