Aerothermodynamic Effects and Modeling of the Tangential Curvature of Guide Vanes in an Axial Turbine Stage

Table 6

The operating points of total pressure at the inlet as a variable in the range of run number between 0.3 and 0.6.

[—]	0.600	0.612	0.672	0.704	0.778	0.800
[Pa]	134543	132957	126460	123753	118911	117797