Solution of Turbine Blade Cascade Flow Using an Improved Panel Method

الملخص EN

An improved panel method has been developed to calculate compressible inviscid flow through a turbine blade row.

The method is a combination of the panel method for infinite cascade, a deviation angle model, and a compressibility correction.

The resulting solution provides a fast flexible mesh-free calculation for cascade flow.

A VKI turbine blade cascade is used to evaluate the method, and the comparison with experiment data is presented.