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Keywords: vertex shroud
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Proceedings Papers
The Thin Ring Wing as a Means of Flow Improvement Upstream a Propeller
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Paper presented at the SNAME 8th Propeller and Shafting Symposium, September 23–24, 1997
Paper Number: SNAME-PSS-1997-16
... can see from that formula the vertex shroud running down from a ring wing is sensitive to the irregularity of the flow upstream : the more intense is the irregularity the greater is the intensity of generated vertices. The vertices intensity may be controlled precisely at any sector of the propeller's...
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