2020
DOI: 10.1017/jfm.2020.145
|View full text |Cite
|
Sign up to set email alerts
|

Vortex moment map for unsteady incompressible viscous flows

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
8
0

Year Published

2020
2020
2024
2024

Publication Types

Select...
6
1

Relationship

2
5

Authors

Journals

citations
Cited by 11 publications
(8 citation statements)
references
References 29 publications
0
8
0
Order By: Relevance
“…Although the aeroservoelastic model developed in this work has similar fidelity as an existing model using a linear vortex panel method (VPM) [31], it can be easily coupled with nonlinear aerodynamic models (e.g. the vortex force [32] and moment [33] map methods developed by us for load estimation in unsteady separating flows)…”
Section: Discussionmentioning
confidence: 99%
“…Although the aeroservoelastic model developed in this work has similar fidelity as an existing model using a linear vortex panel method (VPM) [31], it can be easily coupled with nonlinear aerodynamic models (e.g. the vortex force [32] and moment [33] map methods developed by us for load estimation in unsteady separating flows)…”
Section: Discussionmentioning
confidence: 99%
“…An extension to three-dimensional flows with application to a delta wing was later demonstrated by Li, Zhao & Graham (2020 b ), and the extension to the moment on an aerofoil was demonstrated by Li et al. (2020 a ). This was followed by the treatment of low Reynolds number flows in Li et al.…”
Section: Introductionmentioning
confidence: 92%
“…Moreover, the map provides a visual display of the force-producing and -reducing critical regions and directions. An extension to three-dimensional flows with application to a delta wing was later demonstrated by Li, Zhao & Graham (2020b), and the extension to the moment on an aerofoil was demonstrated by Li et al (2020a). This was followed by the treatment of low Reynolds number flows in Li et al (2021), extending the VFM method to more general cases for a wider range of Reynolds numbers (from O(10) to O(1 × 10 6 )) by adding the viscous-pressure force and skin-friction force contributions to the total force.…”
Section: Introductionmentioning
confidence: 98%
“…More recently, Li et al. (2020 a ) proposed the concept of vortex-moment maps for two dimensional bodies of arbitrary shape to analyse the contribution to the pitching moment from a given vortex in the flow field. In another recent work, a three-dimensional extension of the force-map approach was used by Li, Zhao & Graham (2020 b ) to gain insight into the effect of vortical structures on the unsteady force of a delta wing.…”
Section: Decomposition Of the Leading-edge Suction Parameter (Lesp )mentioning
confidence: 99%