International Journal of Rotating Machinery / 2018 / Article / Tab 2

Research Article

Innovations in Body Force Modeling of Transonic Compressor Blade Rows

Table 2

Design characteristics for NASA stage 67 stator at 90% speed and maximum efficiency.

Parameter ValueParameterValue

number of stator blades 36tip solidity 1.33
aspect ratio 2.160.50
hub solidity 2.570.53

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