2nd AIAA Flow Control Conference 2004
DOI: 10.2514/6.2004-2417
|View full text |Cite
|
Sign up to set email alerts
|
Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
2

Citation Types

2
13
0
1

Year Published

2011
2011
2023
2023

Publication Types

Select...
5
3
1

Relationship

0
9

Authors

Journals

citations
Cited by 20 publications
(16 citation statements)
references
References 10 publications
2
13
0
1
Order By: Relevance
“…The measured lift values are consistent with those described by Schatz et al (2004) in their computational experiments. It is also interesting to point out that these authors subscribe to our perception in considering the influence of features of the wake flow on the wing aerodynamics when they mentioned that particular characteristics of the wake had direct influence upon the increase of the section drag coefficient.…”
Section: Abstract -The Present Research Analyzes the Asymmetry In Thesupporting
confidence: 79%
See 1 more Smart Citation
“…The measured lift values are consistent with those described by Schatz et al (2004) in their computational experiments. It is also interesting to point out that these authors subscribe to our perception in considering the influence of features of the wake flow on the wing aerodynamics when they mentioned that particular characteristics of the wake had direct influence upon the increase of the section drag coefficient.…”
Section: Abstract -The Present Research Analyzes the Asymmetry In Thesupporting
confidence: 79%
“…The wing was examined within the range of -12 degrees and +24 degrees of angle of attack. Airfoils with miniflaps with similar dimensions have been studied by numerical simulations [Schatz et al, 2004]. The lift and drag of a low Reynolds number airfoil HQ17 without and with Gurney flaps of four different lengths: 1%, 1.5%, 2% and 2.5% of the wing chord have been measured.…”
Section: Abstract -The Present Research Analyzes the Asymmetry In Thementioning
confidence: 99%
“…substantially lower than the BL thickness at the TE. Following from that, CFD-based wake simulations of Schatz et al (2004) reveal that the amount of induced drag depends on the GF-height, in fact, in a disproportionate manner, illustrated in Figure 2 (b). As such, for GF = 1.5 %c a vortex street is triggered while for GF = 0.5 %c the wake is shed in a relatively smooth way.…”
Section: Introductionmentioning
confidence: 75%
“…In order to attain a drag reduction by "stabilizing the wake" some authors suggest the use of span-wise holes, slits, serrated flaps and wake-bodies [10], [11], while other recommend to eliminate straightforward the double row of counter-rotating vortices of the wake behind a Gurney type miniflap [12].…”
Section: Introductionmentioning
confidence: 99%