2004
DOI: 10.1115/1.1669432
|View full text |Cite
|
Sign up to set email alerts
|

Low-Speed Aerodynamics, Second Edition

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
18
0

Year Published

2008
2008
2022
2022

Publication Types

Select...
4
2

Relationship

0
6

Authors

Journals

citations
Cited by 17 publications
(21 citation statements)
references
References 0 publications
0
18
0
Order By: Relevance
“…When the foils are vertically separated far enough (RL=2.0C), the wake vortices behind the foils do not interact with each other. The mutual interaction of wake vortices is a function of the distance between the vortices because the induced velocity from the other vortices is proportional to 1/r [18]. The wake patterns in CASE A show the mushroom heads of both upper and lower rows pointing in the same direction, whereas the wake patterns in CASE B show the mushroom heads of the upper and lower rows pointing in the opposite direction with respect to each other.…”
Section: Resultsmentioning
confidence: 97%
See 1 more Smart Citation
“…When the foils are vertically separated far enough (RL=2.0C), the wake vortices behind the foils do not interact with each other. The mutual interaction of wake vortices is a function of the distance between the vortices because the induced velocity from the other vortices is proportional to 1/r [18]. The wake patterns in CASE A show the mushroom heads of both upper and lower rows pointing in the same direction, whereas the wake patterns in CASE B show the mushroom heads of the upper and lower rows pointing in the opposite direction with respect to each other.…”
Section: Resultsmentioning
confidence: 97%
“…It is assumed that the viscous effect is confined within a thin boundary layer. Thus, the flow is assumed to be inviscid, incompressible and irrotational over the entire flow field, excluding the foils' boundaries and their wakes [18].…”
Section: Unsteady Panel Methodsmentioning
confidence: 99%
“…The doublet and source strengths are defined as Katz and Plotkin (2001) give more details about the derivation of these expressions. Eq.…”
Section: Unsteady 3d Surface Panel Methodsmentioning
confidence: 99%
“…Adding the external and kinematic velocity contributions, the total local velocity is Q V Ω r v v = − × − + v . The time-dependent pressure, p k , at the kth panel can be estimated from (Katz and Plotkin, 2001) …”
Section: Unsteady 3d Surface Panel Methodsmentioning
confidence: 99%
See 1 more Smart Citation