Additively Manufactured Compressor Inlet Guide Vane with Fluidic Separation Control

Project number: 
Honeywell Aerospace
Academic year: 
This project will require Capstone team use of the UofA 3D metal printing laboratory and the UofA Aerolab Educational Wind Tunnel facility, including access to the high pressure air supply in the wind tunnel facility.
The team must have access to Computer Aided Design (CAD), Finite Element Analysis (FEA), and Computational Fluid Dynamics (CFD) software.
Weekly (virtual) team meetings.

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