New Results in Numerical and Experimental Fluid Mechanics III 2002
DOI: 10.1007/978-3-540-45466-3_8
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The Relationship Between Near- and-Far-Field of Vortex Wakes from Aircraft with High Aspect Ratio Wings

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Cited by 4 publications
(2 citation statements)
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“…This dependency cannot be shown due to the coupling between circulation and span ratio in the chosen model set-up. Following Stuff [26], slightly stronger flap vortices are needed for lower span ratios. Furthermore, due to the criteria used in this work to characterise the wake vortex alleviation, the limiting circulation ratio Γ 2 /Γ 4 > −0.29 differs from the values (Γ 2 /Γ 4 > −0.2) given by Stuff [26].…”
Section: Outboard Flaps -Conclusionmentioning
confidence: 99%
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“…This dependency cannot be shown due to the coupling between circulation and span ratio in the chosen model set-up. Following Stuff [26], slightly stronger flap vortices are needed for lower span ratios. Furthermore, due to the criteria used in this work to characterise the wake vortex alleviation, the limiting circulation ratio Γ 2 /Γ 4 > −0.29 differs from the values (Γ 2 /Γ 4 > −0.2) given by Stuff [26].…”
Section: Outboard Flaps -Conclusionmentioning
confidence: 99%
“…24 the limit of the circulation ratio is shown. Stuff [26] shows that this limit is in fact a function of the span ratio. This dependency cannot be shown due to the coupling between circulation and span ratio in the chosen model set-up.…”
Section: Outboard Flaps -Conclusionmentioning
confidence: 99%