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For to be real the condition would be: () The loading coefficient and the rotor inlet calculations are iterated until the condition above are satisfied. After finishing that loop the rotor exit velocity triangle, stagnation and static temperature and pressure and rotor exit diameter and blade height can be calculated. For the guide vanes design; a combination of the geometrical parameters selected from the literature and rotor design were used to calculate the dimension of the guide vanes. Based on the guide vanes inlet diameter and width the geometry of the volute were calculated. 2.2.1- PERFORMANCE PARAMETERS: Table 3 contains the design parameters available in literature for radial turbines design. This section outlines the reasoning behind the choice shown in table 3. The minimum value of occurs when Table 3: Design parameters. Parameter Stage Loading Coefficient ( ) Ratio of axial length to rotor inlet radius( Exit flow coefficient ( ) ) Value 0.8 0.7 0.25 1 0.3 0.3 1.2 0.285 0.12 2 Rotor meridional velocity ratio ( Exit hub to inlet tip radius ratio( Vane chord to rotor inlet diameter( ) ) Vane chord to vane pitch (solidity)( ) Thickness of vane leading edge to vane chord( thickness of vane trailing edge to vane height( Inter-space geometry parameter ( ) ) ) 7PDF Image | Optimised Radial Turbine Design D1.8
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