Expected results and long-term impacts
Scientific publications
Authors: Marina G. Kontoua, Xenofon S. Trompoukisa, Varvara G. Asoutia, Kyriakos C. Giannakogloua
Authors: Marina G. Kontoua, Varvara G. Asoutia, Kyriakos C. Giannakogloua
Multi-Fidelity Modelling of the Effect of Combustor Traverse on High-Pressure Turbine Temperatures
Authors: Carta, M.; Shahpar, S.; Ghisu, T.; Licheri, F.
Combustor Traverse Optimization to Lower High-Pressure Turbine Rotor Temperatures
Authors: Carta, M, Ghisu, T, & Shahpar, S.
Authors: Carta M., Shahpar S., Ghisu T.
Heat Transfer Analysis of Damaged Shrouded High-Pressure Turbine Rotor Blades
Authors: Carta M., Shahpar S., Ghisu T.
A First Assessment of Adjoint Body-Force Modeling Capabilities for Fan Design
Authors: Cyril Dosne, Raphael Barrier, Sébastien Bourasseau, Marco Carini, Rocco Moretti, Jaques Peter
An Adjoint Body-Force Approach for Fully-Coupled Aero-Propulsive Optimizations
Authors: Cyril Dosne, R. Barrier, Sébastien Bourasseau, Marco Carini, Rocco Moretti, Jacques Peter
Authors: Quentin Bennehard, Jacques Peter, Marco Carini
Enhancing Decision Making in MDO through Interactive Visual Analytics on the Web
Authors: Henriques-Gil, Javier and Mejia Parra, Daniel and Simoes, Bruno
Project deliverables
D1.1 Tools for aero-propulsive and aero-acoustic optimisation (WP1; ONERA; Sensitive)
D1.2 Assessment of transition models & their adjoints (WP1; NTUA; Public)
D1.3 DENs to Speed-up MDOs (WP1; NTUA; Public)
D1.4 New capabilities of GEMSEO with examples (WP1; IRT; Public)
D1.5 Assessment of UQ/RDO methods (WP1; UNICA; Public)
D2.1 Deep learning borescope demonstrator on an engine borescope video (WP2; ICL; Sensitive)
D2.2 Instant CFD demonstrator on NACA0012 design and ONERA M6 wing cases (publicly available) (WP2; ICL; Public)
D2.3 ML for supporting improved manufacturing: methods and tools (WP2; ICL; Public)
D3.1 Description of design tasks (WP3; AIRBUS; Sensitive)
D3.2 Automatic design chains for the two suggested aircraft concepts (WP3; ONERA; Sensitive)
D3.3 Multidisciplinary design tools for desining next generation business jet acquainted with NLF HARW (WP3; DAV; Sensitive)
D3.4 Multidisciplinary design tools for designing next generation HARW transport aircraft (WP3; DLR; Sensitive)
D4.1 UHBR test case definition (fan, turbine, and heat exchanger) (WP4; RR; Sensitive)
D4.2 USF test case definition (WP4; ONERA; Sensitive)
D4.3 Multi-fidelity aerodynamic-structural design of UHBR fan blade (WP4; UNICA; Sensitive)
D4.4 Multi-fidelity aero-thermal-structural design of compressor/turbine blades (WP4; UNICA; Sensitive)
D4.5 Aero-acoustic optimisation of isolated USF engine (WP4; SAFRAN; Sensitive)
D4.6 Shape optimisation of wing-engine geometries to reduce contrail formation (WP4; USFD; Sensitive)
D4.7 Coupled aero-propulsive optimisation of USF engine and wing (WP4; ONERA; Sensitive)
D5.1 UQ and RO of airframe parts (WP5; DAV; Sensitive)
D5.2 UQ and RO of engine components (WP5; UNICA; Sensitive)
D6.1 Definition of advanced Heat Exchanger geometry and required boundary condition at various flight conditions (WP6; RR; Sensitive)
D6.2 Definition of the cold CAD fan datum geometry, CMM file Formats and data of the scanned UHB Fan blades and HP Turbine Blades (WP6; RR; Sensitive)
D6.3 Delivery of the first Topology optimised Heat-Exchanger (WP6; OPT; Sensitive)
D6.4 Additive Manufacturing of first heat exchanger design (WP6; IRT; Sensitive)
D6.5 Hi-Fi, Multi-passage (NLH and Non-linear) analysis of the Digital Twin of the Manufactured fan blade (WP6; UNICA; Sensitive)
D7.1 Data Management Plan (WP7; ONERA; Sensitive)
D7.2 PEDR-C (WP7; ERDYN; Sensitive)
D7.3 Communication Kit (WP7; ERDYN; Public)
Timeline of the expected results and long-term technical impacts to be achived during and after the project
Funded by the European Union under the GA number: 101056732. Views and opinions expressed are however those of the author(s) only and do not necessarily reflect those of the European Union. Neither the European Union nor the granting authority can be held responsible for them.
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