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Search results for: AERODYNAMIC OPTIMIZATION

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Search results for: AERODYNAMIC OPTIMIZATION

  • Zespół Mechaniki Płynów i Maszyn Przepływowych

    Turbiny parowe, gazowe, powietrzne, wodne; sprężarki, pompy, mechanika płynów

  • Zespół Systemów Mikroelektronicznych

    * projektowania I optymalizacji układów i systemów mikroelektronicznych * zaawansowane metody projektowania i optymalizacji analogowych filtrów aktywnych * programowanie układów scalonych (FPGA, CPLD, SPLD, FPAA) * układy specjalizowane ASIC * synteza systemów o małym poborze mocy * projektowanie topografii układów i zagadnień kompatybilności elektromagnetycznej * modelowania przyrządów półprzewodnikowych * modelowania właściwości...

  • Zespół Katedry Konstrukcji Maszyn i Pojazdów

    * Badania własności smarów i cieczy technicznych * Badania tarcia i zużycia elementów maszyn - dobór materiałów na współpracu-jące elementy, dobór środków smarowych, dobór alternatywnych materiałów umożliwiających pracę bez smarowania lub przy smarowaniu wodą * Badania diagnostyczne maszyn i urządzeń, badania trwałości i niezawodności * Projektowanie i optymalizacja konstrukcji nietypowych maszyn i urządzeń * Projektowanie urządzeń...

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Search results for: AERODYNAMIC OPTIMIZATION

  • Multiobjective Aerodynamic Optimization by Variable-Fidelity Models and Response Surface Surrogates

    Publication

    - AIAA JOURNAL - Year 2016

    A computationally efficient procedure for multiobjective design optimization with variable-fidelity models and response surface surrogates is presented. The proposed approach uses the multiobjective evolutionary algorithm that works with a fast surrogate model, obtained with kriging interpolation of the low-fidelity model data enhanced by space-mapping correction exploiting a few high-fidelity training points. The initial Pareto...

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  • Fast Multi-Objective Aerodynamic Optimization Using Sequential Domain Patching and Multifidelity Models

    Publication

    - JOURNAL OF AIRCRAFT - Year 2020

    Exploration of design tradeoffs for aerodynamic surfaces requires solving of multi-objective optimization (MOO) problems. The major bottleneck here is the time-consuming evaluations of the computational fluid dynamics (CFD) model used to capture the nonlinear physics involved in designing aerodynamic surfaces. This, in conjunction with a large number of simulations necessary to yield a set of designs representing the best possible...

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  • Constrained aerodynamic shape optimization using neural networks and sequential sampling

    Publication

    - Year 2023

    Aerodynamic shape optimization (ASO) involves computational fluid dynamics (CFD)-based search for an optimal aerodynamic shape such as airfoils and wings. Gradient-based optimization (GBO) with adjoints can be used efficiently to solve ASO problems with many design variables, but problems with many constraints can still be challenging. The recently created efficient global optimization algorithm with neural network (NN)-based prediction...

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  • Aerodynamic Shape Optimization for Delaying Dynamic Stall of Airfoils by Regression Kriging

    Publication

    - Year 2020

    The phenomenon of dynamic stall produce adverse aerodynamic loading which can adversely affect the structural strength and life of aerodynamic systems. Aerodynamic shape optimization (ASO) provides an effective approach for delaying and mitigating dynamic stall characteristics without the addition of auxiliary system. ASO, however, requires multiple evaluations time-consuming computational fluid dynamics models. Metamodel-based...

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  • Multi-fidelity robust aerodynamic design optimization under mixed uncertainty

    Publication
    • H. Shah
    • S. Hosder
    • S. Kozieł
    • Y. Tesfahunegn
    • L. Leifsson

    - AEROSPACE SCIENCE AND TECHNOLOGY - Year 2015

    The objective of this paper is to present a robust optimization algorithm for computationally efficient airfoil design under mixed (inherent and epistemic) uncertainty using a multi-fidelity approach. This algorithm exploits stochastic expansions derived from the Non-Intrusive Polynomial Chaos (NIPC) technique to create surrogate models utilized in the optimization process. A combined NIPC expansion approach is used, where both...

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