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International Journal of Rotating Machinery
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International Journal of Rotating Machinery
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2018
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Article
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Tab 2
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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
Value
Parameter
Value
number of stator blades
36
tip solidity
1.33
aspect ratio
2.16
0.50
hub solidity
2.57
0.53