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Keywords: compressors engines and turbines
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Proceedings Papers

Paper presented at the The Eleventh ISOPE Pacific/Asia Offshore Mechanics Symposium, October 12–14, 2014
Paper Number: ISOPE-P-14-075
... that the critical Reynolds number is approximately 2×10 5 (with a scale factor of 1:15). Lower Reynolds number model blades will show unfavorable aerodynamic performance in the model test. rotor thrust coefficient prototype drag coefficient curve compressors engines and turbines tip speed ratio scale...

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