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Compressors, Gas Dynamics and Gas Turbines - Data Intensity 2 :: Discussion
| 11. | In axial flow compressor, exit flow angle deviation from the blade angle is a function of | |
| A. | blade camber | |
| B. | blade camber and incidence angle | |
| C. | space-chord ratio | |
| D. | blade camber and space-chord ratio | |
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