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Introduction to optimization and multidisciplinary design in aeronautics and turbomachinery - hardcover

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Introduction to optimization and multidisciplinary design in aeronautics and turbomachinery., VKI LS 2012-03, ISBN 13 978-2-87516-032-4

Introduction to optimization and multidisciplinary design in aeronautics and turbomachinery

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  • Introduction to optimization and multidisciplinary design in aeronautics and turbomachinery
  • Introduction to optimization and multidisciplinary design in aeronautics and turbomachinery

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Innovative optimization and design techniques for modern aircraft (manned or UAV/UCAV) and engine systems aiming at maximum performance in a multidisciplinary context (aerodynamic efficiency, safety, drag, losses, weight, strength, heat fluxes, emission, noise, …), are now rapidly moving from research labs to industrial real and virtual platforms. To reach concurrently this level of excellence, emergent optimization methodologies require more and more robust and efficient associated software for a daily use in industrial collaborative design environments.

These proceedings intend to provide the basic concepts and tools behind this technology, both in single discipline (single point or multi point design) and multidisciplinary (fluid-structure interaction, fluid-acoustics, conjugate heat transfer, …) context. Subjects which are treated in detail include: gradient based and steepest descent methods, adjoint methods, one shot or goal oriented methods, evolutionary/differential evolution algorithms on parallel environments, game strategies like Pareto Fronts and Nash Equilibrium, parameterization, surrogate and reduced-order modeling (Radial Basis functions, Artificial Neural Networks, Kriging …), multifidelity modeling approaches, robust design, …

The content of these course notes is oriented towards junior and experienced engineers and researchers involved in the field of multi disciplinary design and looking for innovative numerical solutions - or set of solutions- for complex multi criteria optimization problems.

  • VERSTRAETE, T – von Karman Institute for Fluid Dynamics, Belgium
    Introduction to optimization and multidisciplinary design
  • PIRONNEAU, O. – Université Pierre et Marie Curie, France
    Differentiable shape optimization for fluids
  • VASSBERG, J.C. & JAMESON, A. – The Boeing Company & Stanford University, USA
    Theoretical background for aerodynamic shape optimization
  • GAUGER, N.R. – RWTH Aachen University, Germany
    Adjoint approaches in aerodynamic shape optimization and MDO context, Parts I-III
  • GIANNAKOGLOU, K.C.; PAPADIMITRIOU, D.I.; PAPOUTSIS-KIACHAGIAS, E.M. – National Technical University of Athens, Greece
    The continuous adjoint method: theory and industrial applications
  • GIANNAKOGLOU, K.C.; ASOUTI, V.G.; KYRIACOU, S.A.; TROMPOUKIS, X.S.– National Technical University of Athens, Greece
    Hierarchical, metamodel-assisted evolutionary algorithms, with industrial applications
  • VASSBERG, J.C. & JAMESON, A. – The Boeing Company & Stanford University, USA
    Industrial applications of aerodynamic shape optimization
  • PERIAUX, J.1,; GONZALEZ, L. F.; LEE, D.S. – University of Jyvaskyla, Finland
    Queensland University of Technology (QUT), Australia, 3CIMNE/UPC, Spain
  • MOO methods for multidisciplinary design using parallel evolutionary algorithms, game theory and hierarchical topology: theoretical aspects (part 1)
    GONZALEZ, L.F.; LEE, D.S; PERIAUX, J., KOK, J. – Queensland University of Technology (QUT), Australia, CIMNE/UPC, Spain, University of Jyvaskyla, Finland

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Manufacturer von Karman Institute for Fluid Dynamics

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