ACTIVE STALL ELIMINATION BY AIR INJECTION ONTO THE TIP REGION OF COMPRESSOR BLADES
Adaptation of a Ground Test Facility to Operate a Modern Turbo Jet Engine
AIAA-2007-1305 ASSESSMENT OF NUMERICAL METHODS ON A 3.5 STAGE AXIAL COMPRESSOR
A STUDY OF NONLINEAR EDDY-VISCOSITY MODELS IN A FLOW SOLVER FOR TURBOMACHINERY
CFD-Studien eines Lufteinblasesystems zur Unterdruckung von Verdichterinstabilitaten
Designing Advanced Components for High Bypass Engines
Experimental investigation of unsteady flow phenomena in a three-stage axial compressor
Influence of Inflow Turbulence on Loss Behavior of Highly Loaded LPT Cascades
Numerical prediction of cooling losses in a high-pressure gas turbine airfoil