- C The Design Data Of An Inward Radial Flow Gas Turbine Are As Follows Rotor Inlet Tip Diameter 90 Mm Rotor Oulet Tip D 1 (186.4 KiB) Viewed 30 times
C. The design data of an inward radial flow gas turbine are as follows; Rotor inlet tip diameter 90 mm Rotor oulet tip d
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C. The design data of an inward radial flow gas turbine are as follows; Rotor inlet tip diameter 90 mm Rotor oulet tip d
C. The design data of an inward radial flow gas turbine are as follows; Rotor inlet tip diameter 90 mm Rotor oulet tip diameter 62 mm Rotor outlet hub diameter 25 mm Ratio C2/Ca Ratio U1/Ca (ideal) Blade speed Gas density at impeller exit Determine; i. The dimensionless specific speed of the turbine ii. The volume flow rate at impeller outlet iii. The power developed by the turbine = Take for gas: Specific heat ratio, y specific heat at constant pressure, Cp = 1147 J/kg.K 0.447 0.707 30000 r.p.m. 1.8 kg/m3 1.333, gas constant, R = 287 J/kg.K and (CO3-18 marks)