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flowfield improvement in turbines axial gap partial admission turbines genetic algorithm 3d numerical analysis 1d design
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Why is it important?
partial admission turbines optimization and nemerical analysis
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This page is a summary of: Flow pattern improvement in nozzle-rotor axial gap in impulse turbine, Aircraft Engineering and Aerospace Technology, February 2014, Emerald,
DOI: 10.1108/aeat-09-2012-0146.
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