Third Symposium "Simulation of Wing and Nacelle Stall"
21st - 22nd June 2012, Braunschweig, Germany

INLET AND ENGINE FLOWS

1. Probst, A.; Schulze, S.; Kaehler, C. J.; Radespiel, R.:
   Reynolds-Stress Modelling of Subsonic and Transonic Inlet Stall Compared to Measurements



2. Schulze, S.; Hain, R.; Cierpka, C.; Kaehler, C. J.:
   PIV Measurements in a Compressor Test Rig with Distorted Inflow



3. Spiering, F.:
   Coupling of TAU and TRACE for parallel accurate flow simulations



4. Lesser, A.; Ciorciari, R.; Barthmes, S.; Niehuis, R.:
   Numerical Investigation of the Effect of Inflow Distortions on Transonic Axial Compressor Stages



5. Wartzek, F.; Biela, C.; Pixberg, C.; Schiffer, H.-P.:
   Modification of a compressor test rig for measuring the influence of inlet distortions on the compressor flow



6. Krone, J.-H.; Friedrichs, J.:
   Design of a Fan-Test-Facility with axial flow and crosswind capabilities