Aerodynamic control in axial compressor cascades addresses the complex interaction between blade geometry, endwall flows and three-dimensional vortical structures that govern performance and stability ...

To determine the temperature rise of an existing compressor stage, one must relate the flow Mach numbers and angles contained in equation 5.10 to the geometry, the rotative speed, and any other ...

The axial-flow compressor is one of the most common compressor types in use today. It finds its major application in large gas turbine engines like those that power today's jet aircraft. A cutaway ...