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Session B-13: Axial Compressor - Design Analysis and performance
Time:
Friday, 28/Mar/2025:
10:00am - 12:30pm
Session Chair: Frank Eulitz, von Karman Institute for Fluid Dynamics, Belgium
Location:Bldg. 8130 / Rm. 031
Small Lecture Hall
Session B
Presentations
10:00am - 10:30am ID: ETC2025-135
Variable Amplitude Leading Edge Tubercle Optimization of Rotor 37
Yannik Schulz, Christoph Kuestner, Joop Moritz Kohl, Dajan Mimic
Institute of Turbomachinery and Fluid Dynamics (TFD), Leibniz University Hanover, Germany
10:30am - 11:00am ID: ETC2025-325
A Quasi-Direct Numerical Simulation of a Compressor Blade with Separation Bubbles and Inflow Turbulence.
Guglielmo Vivarelli1, Joao Anderson Isler1, Chris Cantwell1, Francesco Montomoli1, Spencer Sherwin1, Yuri Frey-Marioni2, Marcus Meyer3, Iftekhar Naqavi2, Raul Vazquez-Diaz2
1Imperial College London, United Kingdom; 2Rolls-Royce plc Derby; 3Rolls-Royce Deutschland
11:00am - 11:30am ID: ETC2025-300
Compressor tandem blade: investigation into actuation strategies
Mathias Brach1, Andrea Rocca2, Koen Alfons Hillewaert1,2
1Université de Liège, Belgium; 2Cenaero
11:30am - 12:00pm ID: ETC2025-288
Experimental and numerical characterization of the stable operating range of a highly-loaded axial compressor stage
1von Karman Institute, Turbomachinery and Propulsion Dept., Rhode-St-Genèse, Belgium; 2University of Liège, Aerospace and Mechanical Engineering Dept., Liège, Belgium