Active flow control at a 1.5-stage low-speed research compressor with varying rotor tip clearance
Principal Component Analysis on 3D Scanned Compressor Blades for Probabilistic CFD Simulation
AIAA-2005-1058 BOUNDARY LAYER DEVELOPMENT ON ROTOR BLADES OF A FOUR-STAGE LOW-SPEED AXIAL COMPRESSOR
Penny Gap Effect on Performance and Secondary Flowfield in a Compressor Cascade
Active flow control at a 1.5-stage low-speed research compressor with varying rotor tip clearance
Reduction of Secondary Flow Losses in Turbine Cascades by Leading Edge Modifications at the Endwall
Rotating Instabilities in an Axial Compressor Originating From the Fluctuating Blade Tip Vortex