Effects of Number of Bleed Holes on Shock-Wave/Boundary-Layer Interactions in a Transonic Compressor Stator
Bai Li, Xun Zhou, Lei Luo, Wei Du
Topics & Concepts
BleedBoundary layerTransonicMach numberMechanicsSupersonic speedCascadeMaterials scienceBoundary layer suctionOverall pressure ratioFlow separationBoundary layer thicknessGas compressorTotal pressureAerodynamicsBoundary layer controlPhysicsThermodynamicsChemistryMedicineSurgeryChromatographyFluid Dynamics and Turbulent FlowsAerodynamics and Fluid Dynamics ResearchTurbomachinery Performance and Optimization