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For a micro partial admission impulse turbine design, the present study analyzed the variable working conditions by numerical methods. The results indicate that the impact loss on the blade cascades will increase under off-design rotational speeds; the influence of admission fraction on the inner efficiency is decreasing gradually with the nozzle number increasing, and the designed turbine can provide a large scale of output powers by changing the nozzle numbers.

Simulation of Micro Partial Admission Impulse Turbine