(НТУ "ХПИ", 2011) Хомылев, С. А.; Руденко, В. Т.; Люсина, А. В.
The article represents results of investigation of leading edge shape influence on aerodynamic efficiency of high-loaded turbine cascade. The investigation are executed by calculated method for 2D viscous compressible gas flow using the CFD code FlowER. The advices for design of high-loaded profile are given.
