Effect of a blade end slot on supersonic compressor cascade hub-corner separation
Jianci Ma, Guang Yang, Ling Zhou, Lucheng Ji, Chun Zhang
Topics & Concepts
CascadeMechanicsGas compressorBoundary layer suctionFlow separationBoundary layerSupersonic speedSuctionTotal pressurePressure gradientShock (circulatory)Shock waveLeading edgeStatic pressureBoundary layer controlAdverse pressure gradientSeparation (statistics)Position (finance)Axial compressorMaterials sciencePhysicsAerospace engineeringEngineeringComputer scienceMeteorologyChemical engineeringMachine learningInternal medicineMedicineEconomicsFinanceTurbomachinery Performance and OptimizationComputational Fluid Dynamics and AerodynamicsAerodynamics and Fluid Dynamics Research