ERD

A numerical investigation on direct and data-driven flutter prediction methods

Project: RHEA

Updated at: 30-05-2024

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Project acronym RHEA

Geometrically Nonlinear Effects on the Aeroelastic Response of a Transport Aircraft Configuration

Project: RHEA

Updated at: 30-05-2024

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Project acronym RHEA

Periodic Reporting for period 3 - RHEA (Robust- and sustainable-by-design ultra-higH aspEct ratio wing and Airframe)

Project: RHEA

Updated at: 01-04-2024

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Project acronym RHEA

Report on estimated environmental impact of SBW and associated implications with regulatory framework, technology road m...

Project: RHEA

Updated at: 05-03-2024

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Project acronym RHEA

Report on the preliminary design approach and the six initial architectures, MDO of the mid-range configuration

Project: RHEA

Updated at: 05-03-2024

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Project acronym RHEA

Dissemination and Communication Plan

Project: RHEA

Updated at: 05-03-2024

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Project acronym RHEA

Report on final assessment of SBW

Project: RHEA

Updated at: 05-03-2024

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Project acronym RHEA

Initial Weight Estimation of Twin-Fuselage Configuration in Aircraft Conceptual Design

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

A Geometrically Nonlinear Structural Model for Aerostructural Optimization of Ultra-High Aspect Ratio Composite Wings

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Polynomial preconditioning in unsteady aerodynamic models for aeroelasticity

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Multi-fidelity Nonlinear Aeroelastic Analysis of a Strut-braced Ultra-high Aspect Ratio Wing Configuration

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Comprehensive approach for aerostructural optimisation of ultra-high aspect ratio wings

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Computational Challenges in the Modular Design of Future Aircraft Concepts with Flutter Constraints

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Session 6: Enabling technologies

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Adaptive Data-Driven Model Order Reduction for Unsteady Aerodynamics

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Next steps in aerostructural design of ultra-high aspect ratio wings

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Geometric sensitivity study on the aerodynamics of a strut-braced wing

Project: RHEA

Updated at: 06-02-2024

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Project acronym RHEA

Report on methods for uncertainty quantification

Project: RHEA

Updated at: 31-10-2023

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Project acronym RHEA

Investigating the Influence of Uncertainty in Novel Airframe Technologies on Realizing Ultra-high Aspect Ratio Wings

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

A non-intrusive nonlinear aeroelastic extension of loads packages with application to long range transport aircraft conf...

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Report on the aeroelastic coupled aerostructural modelling methodologies and associated open-source implementations

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Project plan

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Conceptual design and comparative study of strut-braced wing and twin-fuselage aircraft configurations with ultra-high a...

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Literature study report

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Data Management Plan

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Conceptual Design and Comparative Study of Strut-Braced Wing and Twin-Fuselage Aircraft Configurations with Ultra-High A...

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Conceptual design and comparative study of strut-braced wing and twin-fuselage aircraft configurations with ultra-high a...

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Twin-fuselage configuration for improving fuel efficiency of passenger aircraft

Project: RHEA

Updated at: 31-07-2023

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Project acronym RHEA

Resources

Selected filters:

A numerical investigation on direct and data-driven flutter prediction methods

Geometrically Nonlinear Effects on the Aeroelastic Response of a Transport Aircraft Configuration

Periodic Reporting for period 3 - RHEA (Robust- and sustainable-by-design ultra-higH aspEct ratio wing and Airframe)

Report on estimated environmental impact of SBW and associated implications with regulatory framework, technology road m...

Report on the preliminary design approach and the six initial architectures, MDO of the mid-range configuration

Dissemination and Communication Plan

Report on final assessment of SBW

Initial Weight Estimation of Twin-Fuselage Configuration in Aircraft Conceptual Design

A Geometrically Nonlinear Structural Model for Aerostructural Optimization of Ultra-High Aspect Ratio Composite Wings

Polynomial preconditioning in unsteady aerodynamic models for aeroelasticity

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Multi-fidelity Nonlinear Aeroelastic Analysis of a Strut-braced Ultra-high Aspect Ratio Wing Configuration

Comprehensive approach for aerostructural optimisation of ultra-high aspect ratio wings

Computational Challenges in the Modular Design of Future Aircraft Concepts with Flutter Constraints

Session 6: Enabling technologies

Adaptive Data-Driven Model Order Reduction for Unsteady Aerodynamics

Next steps in aerostructural design of ultra-high aspect ratio wings

Geometric sensitivity study on the aerodynamics of a strut-braced wing

Report on methods for uncertainty quantification

Investigating the Influence of Uncertainty in Novel Airframe Technologies on Realizing Ultra-high Aspect Ratio Wings

A non-intrusive nonlinear aeroelastic extension of loads packages with application to long range transport aircraft conf...

Report on the aeroelastic coupled aerostructural modelling methodologies and associated open-source implementations

Project plan

Conceptual design and comparative study of strut-braced wing and twin-fuselage aircraft configurations with ultra-high a...

Literature study report

Data Management Plan

Conceptual Design and Comparative Study of Strut-Braced Wing and Twin-Fuselage Aircraft Configurations with Ultra-High A...

Data-driven Adaptive Model Order Reduction Framework for Aerodynamics

Conceptual design and comparative study of strut-braced wing and twin-fuselage aircraft configurations with ultra-high a...

Twin-fuselage configuration for improving fuel efficiency of passenger aircraft