CoFAS Compressor and Fan Aeroelasticity and Stability limits

Important results from the project

Engines using BLI (Boundary Layer Ingestion) have a significant potential to reduce fuel consumption of future aircraft and is an example of a technology where the engine operates in significant distortion. The CoFAS goal is to improve capabilities for analysis of conditions that occur in operation as well as to enable optimized designs. Models and design methods are developed in the project using advanced analysis tools for simulation of aeroelasticity with distorted inlets.

Expected long term effects

The focus of the project lies on numerical models. In order to validate the theoretical findings, collaborations have been formed for with partners having common interests and unique test capabilities that are suited for the validation. The learnings from analyses and tests have been used to propose designs that are suitable for future more efficient propulsion with lower environmental impact.

Approach and implementation

Available numerical models have been used to analyse compressor and fans. A design proposed for a demonstrator of a boundary layer ingesting fan was introduced for developing the models. Test objects have been designed and tested in collaboration with partners in order to validate the models and the fan designs. Publications of the findings have resulted in seven peer reviewed conference papers and journal articles.