SoftInWay - Conceptual turbomachinery design and optimization
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Initial turbine design data presented in table 1 and flow path sketch is presented below.

Table 1

Initial design data

1 total pressure at inlet Pa 533293
2 total enthalpy at inlet J/kg 1203438 
3 total temperature at inlet K 1103 
4 stat. pressure at outlet Pa 172000 
5   mass flow rate at inlet   kg/s   91.91575 
6 inlet flow angle in abs frame deg 90
7 isentropic velocity ratio - 0.504
8 capacity MW 22.79
9 total-static pressure ratio - 3.015
10 axial length m 0.42


Figure 3. Initial turbine design

Figure 3. Initial turbine design

Counter-rotating Design (4 stages). Counter-rotating turbine design procedure was performed in the following way: the vanes of the initial turbine were removed, and the number of stages was kept in the counter-rotating turbine as in the prototype. We assume that the most correct comparison of two designs could be made only in this case. In the figure below counter-rotating turbine flow path obtained after redesign is presented. Blades which are joined to the first and the second shafts are colored red and purple colors correspondingly.



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