ERD

A Search for the “ULTIMATE” Aero-Engine

Project: ULTIMATE

Updated at: 11-05-2024

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Multi-disciplinary Assessments of Novel Propulsion Technologies for Civil Aviation: Technoeconomic Enviromental Risk Ass...

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Lessons from Advanced Concept Studies in EU Framework Programmes

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Performance of a Supercritical CO2 Bottoming Cycle for Aero Applications

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ULTIMATE public web site

Project: ULTIMATE

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Investigation and Assessment of the Performance of Various Recuperative Cycles Based on the Intercooled Recuperation Con...

Project: ULTIMATE

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Efficient Optimization of Recuperator Design for Aero Engine Applications

Project: ULTIMATE

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The effect of turbine blade cooling on the performance of recuperative cycles for gas turbines applications

Project: ULTIMATE

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Performance and Preliminary Design of Combined Cycle Aero Engines utilising Supercritical Carbon Dioxide

Project: ULTIMATE

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3D LES - RANS CFD Studies of a Novel Secondary Combustor Concept for Low-NOx Emissions

Project: ULTIMATE

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Preliminary Design and Emissions Evaluation of an Aero Engine Secondary Combustor

Project: ULTIMATE

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Design Optimization of Heat Exchangers for Aero Engines With the Use of a Surrogate Model Incorporating Performance Char...

Project: ULTIMATE

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Investigations of the synergy of Composite Cycle and intercooled recuperation

Project: ULTIMATE

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Conceptual design study of a geared turbofan and an open rotor aero engine with intercooled recuperated core

Project: ULTIMATE

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Project acronym ULTIMATE

Investigations of Synergistic Combination of the Composite Cycle and Intercooled Recuperation

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Scale Effects on Conventional and Intercooled Turbofan Engine Performance

Project: ULTIMATE

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Investigation and Design of Power Transmission Systems for Novel Propulsion Technologies

Project: ULTIMATE

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Project acronym ULTIMATE

Assessment of CO2 and NOx emissions in intercooled pulsed detonation turbofan engines

Project: ULTIMATE

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A Composite Cycle Engine Concept for Year 2050

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3D URANS Study of a Nutating Disc Engine Compressor

Project: ULTIMATE

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Ultra Low Emission Technology Innovations for Mid-Century Aircraft Turbine Engines

Project: ULTIMATE

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Project acronym ULTIMATE

ULTIMATE - Ultra Low emission Technology Innovations for Mid-century Aircraft Turbine Engines

Project: ULTIMATE

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Advanced Tube and Wing Aircraft for Year 2050 Timeframe

Project: ULTIMATE

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Validating the Harmonic Balance Method for Turbomachinery Tonal Noise Predictions

Project: ULTIMATE

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Public Workshop

Project: ULTIMATE

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Project acronym ULTIMATE

The efficiency of a pulsed detonation combustor–axial turbine integration

Project: ULTIMATE

Updated at: 11-05-2024

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Project acronym ULTIMATE

Assessment of CO 2 and NO x Emissions in Intercooled Pulsed Detonation Turbofan Engines

Project: ULTIMATE

Updated at: 11-05-2024

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Analytical Model for the Performance Estimation of Pre-Cooled Pulse Detonation Turbofan Engines

Project: ULTIMATE

Updated at: 11-05-2024

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Implementation of a Quasi-Three-Dimensional Nonreflecting Blade Row Interface for Steady and Unsteady Analysis of Axial ...

Project: ULTIMATE

Updated at: 11-05-2024

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Aeroacoustic Analysis of a Counter Rotating Open Rotor based on the Harmonic Balance Method

Project: ULTIMATE

Updated at: 11-05-2024

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