Effect of Inlet Distortions, Co-Swirl and Counter-Swirl on...
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Paper presents an inlet flow distortion study on a single axial fan and a contra-Rotating Twin rotor axial fan. A significant outcome is that in spite of a higher distortion, counter-swirl produces a lower degradation in performance compared to the co-swirl, which has lower distortion intensity. Also, the performance penalty in the case of the contra-rotating unit is less as compared to the single axial fan.
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Added to
Amit Batra - Aer... folder
on Jun. 23 2007
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| Size: 194.6kb |
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Tags:
Axial
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Fan
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Turbomachinery
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Aerospace
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research
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wind
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tunnel
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Engineering
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Compressors
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Experiment
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Folder Tags:
Fluid
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Mechanics
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Finite
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Difference
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Aerospace
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Engineering
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ASME
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Mechanical
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Instrumentation
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