Loss reduction in a high-speed compressor cascade using an L-shaped endwall groove to generate a streamwise vortex
Bo Wang, Yanhui Wu, Stephen Spence
Topics & Concepts
CascadeVortexReduction (mathematics)Groove (engineering)Gas compressorMechanicsPhysicsWingtip deviceAerospace engineeringMaterials scienceGeometryEngineeringMechanical engineeringMathematicsAerodynamicsChemical engineeringTurbomachinery Performance and OptimizationFluid Dynamics and Turbulent FlowsHeat Transfer Mechanisms