ENOVAL -  Ultra High Bypass Ratio Aero Engines
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      • Ice Impact Testing on IMC
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      • Low Pressure Turbine technology: ITP/CTA test completed
      • Variable Area Fan Nozzle Concept for UHBPR Engines
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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

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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