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Multidisciplinary ADjoint-based Enablers for LArge-scale INdustrial dEsign in aeronautics

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Pubblicazioni

Coupled Adjoint Fluid-Structure Interaction Technique for Flexible Wing Shape Optimization

Autori: Tsiakas, Konstantinos; Roge, Gilbert; Trompoukis, Xenofon; Asouti, Varvara; Fougeron, Gabriel; Julisson, Sarah; Martin, Ludovic; Kleinveld, Steven; Giannakoglou, Kyriakos
Pubblicato in: 14th WCCM & ECCOMAS Congress 2021, 2021
Editore: 14th WCCM & ECCOMAS Congress 2021
DOI: 10.23967/wccm-eccomas.2020.108

Structurally Constrained Aerodynamic Adjoint Optimisation of Highly Loaded Compressor Blades

Autori: Cleopatra Cuciumita, Alistair John, Ning Qin, Shahrokh Shahpar
Pubblicato in: ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition, 2021
Editore: ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition
DOI: 10.1115/gt2021-59717

Low-Noise Blade Design Optimisation for a Transonic Fan Using Adjoint-Based MDO Approach

Autori: Long Wu
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021
DOI: 10.2514/6.2021-3055

On the Benefits of Engaging Coupled-Adjoint to Perform High-Fidelity Multipoint Aircraft Shape Optimization

Autori: Romain Olivanti
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021
DOI: 10.2514/6.2021-3072

Gradient-enhanced least-square Polynomial Chaos expansions in Aeronautics

Autori: Tiziano Ghisu, Diego I. Lopez, Pranay Seshadri, Shahrokh Shahpar
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021
DOI: 10.2514/6.2021-3073

Aggregated Formulation of Geometric Constraints for Node-based Shape Optimization with Vertex Morphing

Autori: Armin Geiser, Ihar Antonau, Kai-Uwe Bletzinger
Pubblicato in: 2021
Editore: ECCOMAS Proceedia
DOI: 10.7712/140121.7952.18383

Multidisciplinary ADjoint-based Enablers for LargE-scale Industrial desigN in aEronautics

Autori: Michaël Méheut
Pubblicato in: EUROGEN 2019, 2019
Editore: EUROGEN 2019

A data-driven scalable MDO problem to compare MDO formulations

Autori: Matthias De Lozzo
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021
DOI: 10.2514/6.2021-3053

Multidisciplinary Optimisation of High Pressure Turbine Blade Tip With Turbine Inlet Capacity and Stage Reaction Constraints

Autori: Luka Vincekovic
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021
DOI: 10.2514/6.2021-3071

Toward An Adjoint Based Aeroacoustic Optimisation For Propeller Noise Reduction

Autori: Alain Chelius, Itham Salah El Din, Régis Koch
Pubblicato in: ICSV26 26th International Congress on Sound & Vibration, 2019
Editore: ICSV26 26th International Congress on Sound & Vibration

Towards industrial aero structural aircraft optimization via coupled adjoint derivatives

Autori: Marco Carini
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021
DOI: 10.2514/6.2021-3074

AI-Assisted Strategies for High Dimensional Optimisation in Turbomachinery

Autori: Diego Lopez, Tiziano Ghisu
Pubblicato in: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data, 2021
Editore: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data

Global Optimization of a Transonic Fan Blade Through AI-Enabled Active Subspaces

Autori: Diego I. Lopez, Tiziano Ghisu, Shahrokh Shahpar
Pubblicato in: Journal of Turbomachinery, 2021
Editore: Journal of Turbomachinery.
DOI: 10.1115/1.4052136

Continuous Adjoint Shape Optimization of Internally Cooled Turbine Blade

Autori: Trompoukis, Xenofon; Tsiakas, Konstantinos; Asouti, Varvara; Kontou, Marina; Giannakoglou, Kyriakos
Pubblicato in: 14th European Conference on Turbomachinery Fluid dynamics & Thermodynamics, 2021
Editore: EUROTURBO
DOI: 10.5281/zenodo.5713531

MADELEINE: Project Overview

Autori: Michaël Méheut
Pubblicato in: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data, 2021
Editore: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data

Mesh Independency Of The Vertex Morphing Method For Gradient-Based Shape Optimisation

Autori: Armin Geiser
Pubblicato in: 14th WCCM & ECCOMAS Congress 2021, 2021
Editore: 14th WCCM & ECCOMAS Congress 2021

MADELEINE Project: Challenges Of Adjoint-Based Multi-Disciplinary Optimisation In Industry

Autori: Michaël Méheut
Pubblicato in: 14th WCCM & ECCOMAS Congress 2021, 2021
Editore: 14th WCCM & ECCOMAS Congress 2021

High-Fidelity Adjoint-Based Multi-Disciplinary Optimisation In The Madeleine Project

Autori: Michaël Méheut
Pubblicato in: EUROGEN 2021, 2021
Editore: EUROGEN 2021

Adjoint-based optimization for a jet-engine fan blade design

Autori: Andrea Giugno
Pubblicato in: EUROGEN 2019, 2019
Editore: EUROGEN 2019

The Influence of Parameterisation Setup on the Constrained Adjoint Optimisation of Transonic Fan Blades

Autori: Alistair John, Ning Qin, Shahrokh Shahpar
Pubblicato in: ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, 2021
Editore: ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition
DOI: 10.1115/gt2020-15352

Aeroacoustic Propeller Design Using High-Fidelity CFD And Ffowcs-Hawkins Analogy

Autori: Bambang Soemarwoto
Pubblicato in: 14th WCCM & ECCOMAS Congress 2021, 2021
Editore: 14th WCCM & ECCOMAS Congress 2021

Pave the way to robust aerostructure wing shape optimization

Autori: Gilbert Rogé
Pubblicato in: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data, 2021
Editore: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data

Comparing Two Multidisciplinary Optimization Formulations of Trimmed Aircraft Subject to Industry-relevant Loads and Constraints

Autori: Mohammed Abu-Zurayk
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021
DOI: 10.2514/6.2021-3075

Evaluation And Comparison Of Mesh Deformation Techniques For Industrial Aerospace Applications

Autori: Alistair John
Pubblicato in: 14th WCCM & ECCOMAS Congress 2021, 2021
Editore: 14th WCCM & ECCOMAS Congress 2021

Continuous Adjoint–based Aeroacoustic Shape Optimization of an Aero–engine Intake

Autori: Monfaredi, Morteza; Asouti, Varvara; Trompoukis, Xenofon; Tsiakas, Konstantinos; Giannakoglou, Kyriakos
Pubblicato in: EUROGEN 2021, 2021
Editore: EUROGEN 2021
DOI: 10.5281/zenodo.5713576

Adjoint-based Aerodynamic Optimization of a Business Jet Flexible Wing

Autori: Konstantinos Tsiakas
Pubblicato in: EUROGEN 2019, 2019
Editore: EUROGEN 2019

A comparison of different formulations for aero-structural optimization of trimmed transport aircraft

Autori: Mohammed Abu-Zurayk
Pubblicato in: EUROEGN 2019, 2019
Editore: EUROGEN 2019

Aggregated formulation of geometric constraints for node-based shape optimization with Vertex Morphing

Autori: Armin Geiser, Ihar Antonau, Kai-Uwe Bletzinger
Pubblicato in: EUROGEN 2021, 2021
Editore: EUROGEN 2021

Continuous Adjoint-based Aerothermal & Aeroacoustic Optimization of Aero Engine Components using PUMA

Autori: Kyriakos C. Giannakoglou
Pubblicato in: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data, 2021
Editore: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data

Multidisciplinary Adjoint-based Optimizations in the MADELEINE Project: Overview and Main Results

Autori: Michaël Méheut
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021
DOI: 10.2514/6.2021-2551

Pave the way to robust aerostructure wing shape optimization

Autori: Gilbert Rogé
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021

Unsteady Adjoint Method for Aeroacoustic Propeller Optimization

Autori: Bambang Soemarwoto
Pubblicato in: AIAA Aviation Forum 2021, 2021
Editore: AIAA Aviation Forum 2021
DOI: 10.2514/6.2021-3054

Exploring Topology Optimisation of High Pressure Turbine Blade Tips

Autori: Luka Vincekovic, Alistair John, Ning Qin, Shahrokh Shahpar
Pubblicato in: ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, 2021
Editore: ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition
DOI: 10.1115/gt2020-16059

Isolated Propeller and a Turbofan Fan Adjoint Based GradientAero-Acoustic Optimisation Within the MADELEINE Project

Autori: Itham Salah El Din
Pubblicato in: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data, 2021
Editore: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data

Multidisciplinary ADjoint-based Enablers for LargE-scale Industrial desigN in aEronautics

Autori: Michaël Méheut
Pubblicato in: 2nd European Workshop on MDO for Industrial Applications in Aeronautics, 2020
Editore: 2nd European Workshop on MDO for Industrial Applications in Aeronautics

CFD based topology optimization for turbine blade tip

Autori: Jack Cundall
Pubblicato in: EUROGEN 2019, 2019
Editore: EUROGEN 2019

The influence of design space choices on the adjoint optimisation of transonic compressor blades

Autori: Alistair John
Pubblicato in: EUROGEN 2019, 2019
Editore: EUROGEN 2019

On the selection of the most appropriate MDO formulation with respect to the problem dimension: application to realistic aerostructure wing design

Autori: Matthias De Lozzo
Pubblicato in: EUROGEN 2019, 2019
Editore: EUROGEN 2019

Comparing the use of Aerodynamic Adjoint and AeroelasticAdjoint in Aeroelastic Optimization of Industry Relevant Aircraft Configuration

Autori: Mohammad Abu Zurayk
Pubblicato in: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data, 2021
Editore: CM3 Workshop - Computational Multi Physics, Multi Scales and Multi Big Data

Low-Noise Blade Design Optimization for a Transonic Fan Using Adjoint-Based Approach

Autori: Long Wu, Alexander George Wilson, Jae Wook Kim, David Radford and Shahrokh Shahpar
Pubblicato in: AIAA Journal, 2021, ISSN 1533-385X
Editore: American Institute of Aeronautics and Astronautics, Inc.
DOI: 10.2514/1.j060959

Continuous Adjoint-Based Optimization of an Internally Cooled Turbine Blade—Mathematical Development and Application

Autori: Xenofon Trompoukis; Konstantinos Tsiakas; Varvara Asouti; Marina Kontou; Kyriakos Giannakoglou
Pubblicato in: International Journal of Turbomachinery, Propulsion and Power, 2021, ISSN 2504-186X
Editore: MDPI
DOI: 10.3390/ijtpp6020020

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