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Project CATANA focuses on understanding instabilities in turbojet technology caused by interactions between aerodynamic, structural, and acoustic factors. It aims to develop a test case for fan stages that will help improve the efficiency and noise reduction of future aircraft designs.
There is increasing evidence that today’s turbojet technology is limited by instabilities arising from non-linear coupling between aerodynamic, aeroelastic and aeroacoustic phenomena.
These multi-physical processes are going to become even more important in future architectures, which utilize Ultra-High-Bypass Ratio and lightweight composite fan designs to reduce greenhouse gas emissions and noise.
However, enormous knowledge gaps currently exist concerning these processes and the resulting stab…
ECOLE CENTRALE DE LYON
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VON KARMAN INSTITUTE FOR FLUID DYNAMICS- VKI
Belgium, Sint-Genesius-Rode
Type: Research institute
Activity type: Research Organisations
SME: Yes
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