1 - 4 of 4 Chapters
[This paper proposes a computational methodology for the aerodynamic shape design of aeronautical configurations, aiming a broad and efficient exploration of the design space. A novel adaptive sampling technique focused on the global optimization problem, the Intelligent Estimation Search with...
[The chapter proposes the application of surrogate-based optimization to the efficient design of aeronautical configurations. The surrogate model consists of the Proper Orthogonal Decomposition of computed aerodynamic flow fields and Radial Basis Functions interpolation to reconstruct the...
[This paper deals with evolutionary algorithms (EAs) assisted by surrogate evaluation models or metamodels (metamodel-assisted EAs, MAEAs) which are further accelerated by exploiting the principal component analysis (PCA) of the elite members of the evolving population. In each generation of the...
[In order to accurately predict the complex nonlinear relationships between the cyclone performance parameters (The Euler and Stokes numbers) and the four significant geometrical dimensions (the inlet section height and width, the vortex finder diameter and the cyclone total height), the support...
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