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

Informazioni relative al progetto

MADELEINE

ID dell’accordo di sovvenzione: 769025

DOI

10.3030/769025

Progetto chiuso

Data della firma CE 18 Maggio 2018

Data di avvio 1 Giugno 2018

Data di completamento 30 Novembre 2021

Finanziato da

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Costo totale

€ 5 815 181,25

Contributo UE

€ 5 815 181,25

Coordinato da

OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
France

CORDIS fornisce collegamenti ai risultati finali pubblici e alle pubblicazioni dei progetti ORIZZONTE.

I link ai risultati e alle pubblicazioni dei progetti del 7° PQ, così come i link ad alcuni tipi di risultati specifici come dataset e software, sono recuperati dinamicamente da .OpenAIRE .

Risultati finali

Websites, patent fillings, videos etc. (2)

Report regarding the Organisation of the symposium and the workshop
Project public website and social networks

Documents, reports (3)

Dissemination action plan
Gender Equity Policy
Communication set

Pubblicazioni

Conference proceedings (39)

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

Non-peer reviewed articles (1)

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

Peer reviewed articles (1)

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