The partners of the MADELEINE project organised two special sessions dedicated to the project on the 4th and 5th of August (Sessions MDO-12 and MDO-18, Topic: Multidisciplinary Design Optimization).

MADELEINE was represented with the following presentations:

• Multidisciplinary Adjoint-based Optimizations in the MADELEINE Project: Overview and Main Results by Michaël Méheut from the French Aerospace Lab, ONERA
• A data-driven scalable MDO problem to compare MDO formulations by Matthias De Lozzo from IRT Saint Exupéry
• Pave the way to robust aerostructure wing shape optimization by Gilbert Rogé from Dassault Aviation
• Unsteady Adjoint Method for Aeroacoustic Propeller Optimization by Bambang Soemarwoto from the Netherlands Aerospace Centre, NLR
  
• Low-Noise Blade Design Optimisation for a Transonic Fan Using Adjoint-Based MDO Approach by Long Wu from the University of Southampton
• Multidisciplinary Optimisation of High Pressure Turbine Blade Tip With Turbine Inlet Capacity and Stage Reaction Constraints by Luka Vincekovic from the University of Sheffield
• On the Benefits of Engaging Coupled-Adjoint to Perform High-Fidelity Multipoint Aircraft Shape Optimization by Romain Olivanti from Airbus Operations
  
• Gradient-enhanced least-square Polynomial Chaos expansionsin Aeronautics by Tiziano Ghisu from the University of Cagliari
• Towards industrial aero structural aircraft optimization via coupled adjoint derivatives by Marco Carini from the French Aerospace Lab, ONERA
  
• Comparing Two Multidisciplinary Optimization Formulations of Trimmed Aircraft Subject to Industry-relevant Loads and Constraints by Mohammed Abu-Zurayk from the German Aerospace Center, DLR