Current modelling capability for engine icing accretion prediction is still limited for App. C. To further validate icing codes in complex engine geometries, it is necessary to perform additional experimental work in relevant geometrical and environmental conditions. Within the frame of ICE GENESIS [1], an experiment has been setup to replicate the condition at the inlet of an engine first stage compressor. This paper describes the choices for the design of the engine compressor model, the setup within the icing wind tunnel and the methodology employed to obtain the results. Additionally, more effort has been focused on obtaining accurate ice shapes using a 3D scanning system. Results of 3D scans are given.
Engine Cascade Rig Design Tests and Results in App C Conditions
Sae Technical Papers
International Conference on Icing of Aircraft, Engines, and Structures ; 2023
2023-06-15
Conference paper
English
Engine Cascade Rig Design Tests and Results in App C Conditions
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