ENOVAL -  Ultra High Bypass Ratio Aero Engines
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Media Centre

  • News & Events
  • Press Material
  • ENOVAL Documentation
  • Editorials
    • Ice Impact Testing on IMC
    • Assessing Engine Technology
    • Power Gearbox for Future Ducted Geared Engine Configurations
    • Low Pressure Turbine technology: ITP/CTA test completed
    • Variable Area Fan Nozzle Concept for UHBPR Engines
  • Learning Modules

Latest News

ENOVAL programme successfully concluded

Published on: 03-06-2019
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Publications

Measurement techniques for mode detection in aeroengine inter-stage sections     

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Latest Articles

ENOVAL Final Technology Brochure available

Published on: 10-14-2018
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Media Centre

This project has received funding from the European Union’s Seventh Framework Programme for research, technological development and demonstration under grant agreement no 604999

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