The MADELEINE project

We provide here the information on the conference presentations prepared by the consortium partners in the framework of the MADELEINE project.

Please note that all peer-reviewed open access publications issued from the MADELEINE project are available in the MADELEINE Community on Zenodo.

MADELEINE: Project Overview

Presenter: Michaël Méheut from the French Aerospace Lab, ONERA

AI-Assisted Strategies for High Dimensional Optimisation in Turbomachinery

Presenter: Diego Lopez and Tiziano Ghisu from the University of Cagliari

Pave the way to robust aerostructure wing shape optimization

Presenter: Gilbert Rogé from Dassault Aviation

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

Presenter: Mohammad Abu Zurayk from the German Aerospace Center, DLR

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

Presenter: Kyriakos C. Giannakoglou from the National Technical University of Athens

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

Presenter: Itham Salah El Din from the French Aerospace Lab, ONERA

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

Presenter: Michaël Méheut from the French Aerospace Lab, ONERA

A data-driven scalable MDO problem to compare MDO formulations

Presenter: Matthias DeLozzo from IRT Saint Exupéry

Pave the way to robust aerostructure wing shape optimization

Presenter: Gilbert Rogé from Dassault Aviation

Unsteady Adjoint Method for Aeroacoustic Propeller Optimization

Presenter: Bambang Soemarwoto from the Netherlands Aerospace Centre, NLR

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

Presenter: Long Wu from the University of Southampton

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

Presenter: Luka Vincekovic from the University of Sheffield

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

Presenter: Romain Olivanti from Airbus Operations

Gradient-enhanced least-square Polynomial Chaos expansions in Aeronautics

Presenter: Tiziano Ghisu from the University of Cagliari

Towards industrial aero structural aircraft optimization via coupled adjoint derivatives

Presenter: Marco Carini from the French Aerospace Lab, ONERA

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

Presenter: Mohammed Abu-Zurayk from the German Aerospace Center, DLR

Multidisciplinary ADjoint-based Enablers for LargE-scale Industrial desigN in aEronautics: Project Overview
Presenter: Michaël Méheut from ONERA

Presenter: Morteza Monfaredi from the National Technical University of Athens

Aggregated formulation of geometric constraints for node-based shape optimization with Vertex Morphing
Presenter: Armin Geiser from Technical University of Munich
Structurally Constrained Aerodynamic Adjoint Optimisation Of Highly Loaded Compressor Blades
Presenter: Cleopatra Cuciumita from the University of Sheffiled

Global Optimisation of a Transonic Fan Blade Through AI Enabled Active Subspaces
Presenter: Diego Lopez from the Università degli Studi diCagliari
  • 12-16 April 2021: 14th European Turbomachinery Conference (ETC14)
Continuous Adjoint Shape Optimization of Internally Cooled Turbine Blade
Presenter: Xenofon Trompoukis (National Technical University of Athens)
MADELEINE Project: Challenges Of Adjoint-Based Multi-Disciplinary Optimisation In Industry
Presenter: Michaël Méheut (ONERA)

Mesh Independency Of The Vertex Morphing Method For Gradient-Based Shape Optimisation
Presenter: Armin Geiser (Technical University of Munich)

Coupled Adjoint Fluid-Structure Interaction Technique For Flexible Wing Shape Optimization
Presenter: Konstantinos Tsiakas (National Technical University of Athens)

Aeroacoustic Propeller Design Using High-Fidelity CFD And Ffowcs-Hawkins Analogy
Presenter: Bambang Soemarwoto (NLR)

Evaluation And Comparison Of Mesh Deformation Techniques For Industrial Aerospace Applications
Presenter: Alistair John (University of Sheffield)
The influence of parametrisation setup on the constrained adjoint optimisation of transonic fan blades
Presenter: Alistair John (University of Sheffield)

Exploring topology optimisation of high pressure turbine blade tips
Presenter: Luka Vincekovic (University of Sheffield)
Least squares approximation-based polynomial chaos expansion for uncertainty quantification and robust optimization in aeronautics
Presenter: Tiziano Ghisu (University of Cagliari)
Multidisciplinary ADjoint-based Enablers for LargE-scale Industrial desigN in aEronautics
Presenter: Michaël Méheut (ONERA)
Multidisciplinary ADjoint-based Enablers for LargE-scale Industrial desigN in aEronautics
Presenter: Michaël Méheut (ONERA)

CFD based topology optimization for turbine blade tip
Presenter: Jack Cundall (University of Sheffield)

The influence of design space choices on the adjoint optimisation of transonic compressor blades
Presenter: Alistair John (University of Sheffield)

A comparison of different formulations for aero-structural optimization of trimmed transport aircraft
Presenter: Mohammed Abu-Zurayk (DLR)

On the selection of the most appropriate MDO formulation with respect to the problem dimension: application to realistic aerostructure wing design
Presenter: Matthias De Lozzo (IRT Saint Exupéery)

High-Fidelity Adjoint-based Aircraft Shape Optimization with Aeroelastic Trimming and Engine Coupling
Presenter: Andrei Merle (DLR)

Adjoint-based Aerodynamic Optimization of a Business Jet Flexible Wing
Presenter: Konstantinos Tsiakas (National Technical University of Athens)

Adjoint-based optimization for a jet-engine fan blade design
Presenter: Andrea Giugno (Rolls Royce)
Toward An Adjoint Based Aeroacoustic Optimisation For Propeller Noise Reduction
Presenter: Alain Chelius (ONERA)