Question: Problem - 2 . 1 0 : A single - stage axial - flow gas turbine is to be tested in a cold rig so

Problem-2.10: A single-stage axial-flow gas turbine is to be tested in a "cold rig" so as to simulate the design-point operation. The two sets of operating conditions are:
\table[[1. Design - point operation of turbine],[Stage - inlet total pressure,,p01=11bar
Problem - 2 . 1 0 : A single - stage axial - flow

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