《Table 1 Parameters of the transonic high-pressure turbine》

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《Effect of Bowed/Leaned Vane on the Unsteady Aerodynamic Excitation in Transonic Turbine》

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The unsteady computations are performed on a singlestage high pressure turbine of a low bypass ratio aeroengine.This turbine is designed to operate at transonic conditions with a design vane exit Mach number of 1.27at 15217 r/min rotor speed，and the corresponding Reynolds number is 1.6×106.The detailed parameters of the transonic high-pressure turbine are listed in Table 1.