2014
DOI: 10.1139/cjp-2013-0446
|View full text |Cite
|
Sign up to set email alerts
|

Nonlinear electroviscoelastic potential flow instability theory of two superposed streaming dielectric fluids

Abstract: The nonlinear electrohydrodynamic Kelvin-Helmholtz instability of two superposed viscoelastic Walters B= dielectric fluids in the presence of a tangential electric field is investigated in three dimensions using the potential flow analysis. The method of multiple scales is used to obtain a dispersion relation for the linear problem, and a nonlinear Ginzburg-Landau equation with complex coefficients for the nonlinear problem. The linear and nonlinear stability conditions are obtained and discussed both analytic… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

1
3
0

Year Published

2017
2017
2021
2021

Publication Types

Select...
4

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
(4 citation statements)
references
References 32 publications
1
3
0
Order By: Relevance
“…El has a stabilizing influence on the considered system in the occurrence of a vertical electric field. This result is in conformity with that which was gained earlier by El-Sayed et al [38].…”
supporting
confidence: 94%
See 1 more Smart Citation
“…El has a stabilizing influence on the considered system in the occurrence of a vertical electric field. This result is in conformity with that which was gained earlier by El-Sayed et al [38].…”
supporting
confidence: 94%
“…To this end, our interest focuses on the inequality of Equation (38). For this objective, the potential Bond number 2  Log will be designed against the wavenumber k of the surface waves.…”
mentioning
confidence: 99%
“…For recent surveys regarding the developments of linear and nonlinear electromagnetic flows in porous media, see refs. [26][27][28][29][30][31][32][33][34][35][36].…”
Section: Introductionmentioning
confidence: 99%
“…With the increase of the flight speed of modern flight vehicles, panel flutter, a localized aeroelastic problem representing a small portion of the skin on the surface of hypersonic vehicles, is attracting more and more attentions. Many researches have been done in the analysis of panel flutter in supersonic flow (Ma < 5) using the linear aerodynamic theory such as the first-order piston theory [1][2][3][4][5] or linearized potential flow theory [6][7][8]. Particularly, Carrera and his coworkers applied a finite element structural model coupling with first-order piston theory for aerodynamic model to calculate the flutter boundaries of curved panels [9] and versatile thermal insulation (VTI) panels with pinched boundary conditions [10,11].…”
Section: Introductionmentioning
confidence: 99%