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The initial development of a jet caused by fluid, body and free surface interaction with a uniformly accelerated advancing orretreating plate. Part 1. The principal flow

Published online by Cambridge University Press:  20 February 2018

M. T. Gallagher
Affiliation:
School of Mathematics, University of Birmingham, Birmingham B15 2TT, UK
D. J. Needham*
Affiliation:
School of Mathematics, University of Birmingham, Birmingham B15 2TT, UK
J. Billingham
Affiliation:
School of Mathematical Sciences, The University of Nottingham, University Park, Nottingham NG7 2RD, UK
*
Email address for correspondence: d.j.needham@bham.ac.uk

Abstract

The free surface and flow field structure generated by the uniform acceleration (with dimensionless acceleration  $\unicode[STIX]{x1D70E}$ ) of a rigid plate, inclined at an angle $\unicode[STIX]{x1D6FC}\in (0,\unicode[STIX]{x03C0}/2)$ to the exterior horizontal, as it advances ( $\unicode[STIX]{x1D70E}>0$ ) or retreats ( $\unicode[STIX]{x1D70E}<0$ ) from an initially stationary and horizontal strip of inviscid incompressible fluid under gravity, are studied in the small-time limit via the method of matched asymptotic expansions. This work generalises the case of a uniformly accelerating plate advancing into a fluid as studied by Needham et al. (Q. J. Mech. Appl. Maths, vol. 61 (4), 2008, pp. 581–614). Particular attention is paid to the innermost asymptotic regions encompassing the initial interaction between the plate and the free surface. We find that the structure of the solution to the governing initial boundary value problem is characterised in terms of the parameters $\unicode[STIX]{x1D6FC}$ and $\unicode[STIX]{x1D707}$ (where $\unicode[STIX]{x1D707}=1+\unicode[STIX]{x1D70E}\tan \unicode[STIX]{x1D6FC}$ ), with a bifurcation in structure as $\unicode[STIX]{x1D707}$ changes sign. This bifurcation in structure leads us to question the well-posedness and stability of the governing initial boundary value problem with respect to small perturbations in initial data in the innermost asymptotic regions, the discussion of which will be presented in the companion paper Gallagher et al. (J. Fluid Mech. vol. 841, 2018, pp. 146–166). In particular, when $(\unicode[STIX]{x1D6FC},\unicode[STIX]{x1D707})\in (0,\unicode[STIX]{x03C0}/2)\times \mathbb{R}^{+}$ , the free surface close to the initial contact point remains monotone, and encompasses a swelling jet when $(\unicode[STIX]{x1D6FC},\unicode[STIX]{x1D707})\in (0,\unicode[STIX]{x03C0}/2)\times [1,\infty )$ or a collapsing jet when $(\unicode[STIX]{x1D6FC},\unicode[STIX]{x1D707})\in (0,\unicode[STIX]{x03C0}/2)\times (0,1)$ . However, when $(\unicode[STIX]{x1D6FC},\unicode[STIX]{x1D707})\in (0,\unicode[STIX]{x03C0}/2)\times \mathbb{R}^{-}$ , the collapsing jet develops a more complex structure, with the free surface close to the initial contact point now developing a finite number of local oscillations, with near resonance type behaviour occurring close to a countable set of critical plate angles $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x1D6FC}_{n}^{\ast }\in (0,\unicode[STIX]{x03C0}/2)$ ( $n=1,2,\ldots$ ).

Information

Type
JFM Papers
Creative Commons
Creative Common License - CCCreative Common License - BY
This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted re-use, distribution, and reproduction in any medium, provided the original work is properly cited.
Copyright
© 2018 Cambridge University Press
Figure 0

Figure 1. Definition sketch showing the displacement of the plate and free surface at time $t$.

Figure 1

Figure 2. Equipotentials of $\overline{\unicode[STIX]{x1D719}}$ when $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$. Lines separate regions in which (3.5), (3.6) or (3.7) is used.

Figure 2

Figure 3. The free surface elevation $\overline{\unicode[STIX]{x1D702}}$, scaled with respect to $\unicode[STIX]{x1D70E}$. A circle highlights the transition from (3.8) to (3.9).

Figure 3

Figure 4. The coefficient $A_{0}$ plotted against $\unicode[STIX]{x1D6FC}$. The solid line shows the analytical expression (3.10), while numerical approximations are shown as dots.

Figure 4

Figure 5. Contours of $\unicode[STIX]{x1D6F7}$ for the numerical solution of $\text{(PBVP)}^{+}$ when $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$ and $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/6$. In each plot, a black line shows $\widehat{R}=2.5$, after which the far-field asymptotic form (4.25) is plotted.

Figure 5

Figure 6. Contours of $\unicode[STIX]{x1D6F7}$ for the exact solution (4.31) of $\text{(PBVP)}^{+}$ when $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$ and $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/6$.

Figure 6

Figure 7. Graphs of $H$ for the numerical solution of $(\text{PBVP})^{+}$ for a selection of angles $\unicode[STIX]{x1D6FC}$. In each graph, a square shows $\widehat{R}=2.5$, after which the far-field asymptotic form (4.20) is plotted.

Figure 7

Figure 8. Numerical approximation to $H(0)$ and $H_{\widehat{X}}(0)$ for $(\text{PBVP})^{+}$. Exact values for $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x1D6FC}_{n}$ ($n=1,2,\ldots ,10$) (via (4.32)) are shown as circles.

Figure 8

Figure 9. Numerical approximation to the near-field constant $a_{0}(\unicode[STIX]{x1D6FC})$ for $(\text{PBVP})^{+}$. Exact solutions for $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x1D6FC}_{n}$ ($n=1,2,\ldots ,10$) (4.34) are shown as circles.

Figure 9

Figure 10. Contours of $\unicode[STIX]{x1D6F7}$ for the numerical solution of $\text{(PBVP)}^{-}$ when $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$ and $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/6$. In each plot, a line shows $\widehat{R}=10$, after which the far-field asymptotic form (4.25) is plotted.

Figure 10

Figure 11. Graphs of $H$ for the numerical solution of $\text{(PBVP)}^{-}$ when $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$ and $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/6$. In each plot, a square shows $\widehat{R}=10$, after which the far-field asymptotic form (4.20) is plotted.

Figure 11

Figure 12. Contours of $\unicode[STIX]{x1D6F7}$ for the numerical solution of $\text{(PBVP)}^{-}$ close to the tip of the wedge when (a$\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$ and (b$\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/6$. The stationary points are marked with a dot. It should be noted that the scales in (b)(i) and (b)(ii) have been chosen to show clearly the contours of $\unicode[STIX]{x1D6F7}$ close to each of the stationary points.

Figure 12

Figure 13. Graphs of $H$ close to the tip of the wedge for the numerical solution of $\text{(PBVP)}^{-}$ when $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$ and $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/6$. In each plot, circles highlight the locations of zeros of $H$.

Figure 13

Figure 14. The vector field $\widehat{\unicode[STIX]{x1D735}}\unicode[STIX]{x1D6F7}$ for the numerical solution of $\text{(PBVP)}^{-}$ close to the tip of the wedge when (a$\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$ and (b$\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/6$. The reversal points are marked with a dot. It should be noted that the scales in (b) have been chosen to show clearly the vector field $\widehat{\unicode[STIX]{x1D735}}\unicode[STIX]{x1D6F7}$ close to each of the reversal points.

Figure 14

Figure 15. Contours of $\unicode[STIX]{x1D6F7}$ for the exact solution (4.31) of $\text{(PBVP)}^{-}$ when $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$ and $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/6$.

Figure 15

Figure 16. Graphs of $H$ for the exact solution (4.32) of $\text{(PBVP)}^{-}$ when $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/4$ and $\unicode[STIX]{x1D6FC}=\unicode[STIX]{x03C0}/6$.

Figure 16

Figure 17. A qualitative sketch of the structure of $a_{0}(\unicode[STIX]{x1D6FC})$ for $\unicode[STIX]{x1D6FC}\in (0,\unicode[STIX]{x03C0}/2)$.

Figure 17

Figure 18. Contour plot of $t^{2-\unicode[STIX]{x03C0}/\unicode[STIX]{x1D6FC}}\unicode[STIX]{x1D702}_{\overline{x}}(\overline{X}_{p}(t),t)$ as $t\rightarrow 0^{+}$ on the $(\unicode[STIX]{x1D6FC},\unicode[STIX]{x1D707})$ plane, in the case $\unicode[STIX]{x1D707}>0$.

Figure 18

Figure 19. Contour plots of $t^{2-\unicode[STIX]{x03C0}/\unicode[STIX]{x1D6FC}}\unicode[STIX]{x1D702}_{\overline{x}}(\overline{X}_{p}(t),t)$ as $t\rightarrow 0^{+}$ on the $(\unicode[STIX]{x1D6FC},\unicode[STIX]{x1D707})$ plane in the case $\unicode[STIX]{x1D707}<0$ with $\unicode[STIX]{x1D6FC}\in (\unicode[STIX]{x1D6FC}_{1}^{\ast },\unicode[STIX]{x03C0}/\unicode[STIX]{x1D6FC})$ and $\unicode[STIX]{x1D6FC}\in (\unicode[STIX]{x1D6FC}_{n+1}^{\ast },\unicode[STIX]{x1D6FC}_{n}^{\ast })$ ($n=1,2,\ldots ,5$).

Figure 19

Figure 20. Graph of the free surface function $\widehat{H}(\widehat{x})$ against $\widehat{x}$, showing agreement with the far-field asymptotic form (5.16), for the numerical solution of (RBVP) with $\unicode[STIX]{x1D6FC}=0.9$, 1, 1.1, 1.2, 1.3, 1.4, 1.5 and 1.56. For each angle, a square shows $s=250$, after which the far-field asymptotic form (5.16) is plotted, and a dashed line shows the location of the plate.

Figure 20

Figure 21. Graphs of $\widehat{H}(\widehat{x})$ against $\widehat{x}$ for the numerical solution of (RBVP). (a) Solutions with $\unicode[STIX]{x1D6FC}=0.9$, 1, 1.1, 1.2, 1.3, 1.4, 1.5 and 1.56; (b) solutions close to the plate with $\unicode[STIX]{x1D6FC}=1.1$, 1.2, 1.3, 1.4, 1.5 and 1.56 for clarity. For each angle, a dashed line shows the location of the plate.

Figure 21

Figure 22. Numerical approximations to $\widehat{x}_{0}(\unicode[STIX]{x1D6FC})$, $\widehat{H}(\widehat{x}_{0}(\unicode[STIX]{x1D6FC}))$ and $\widehat{H}_{\widehat{x}}(\widehat{x}_{0}(\unicode[STIX]{x1D6FC}))$ for (RBVP). In (c), the curve $\tan (\unicode[STIX]{x03C0}/2-\unicode[STIX]{x1D6FC})$ is plotted as a solid line, with numerical approximations shown as crosses.

Figure 22

Figure 23. Graph showing the distance in the $(\widehat{x},\widehat{y})$ coordinate system from the origin of the $(\widehat{x},\widehat{y})$ coordinate system to the contact point of the free surface and the plate against $\unicode[STIX]{x1D6FC}\in (\unicode[STIX]{x03C0}/4,\unicode[STIX]{x03C0}/2)$, as determined by the numerical solution of (RBVP).

Figure 23

Figure 24. The free surface close to the plate when $\unicode[STIX]{x1D6FC}=1.56$. It should be noted that the axes have been rotated so that the plate lies along the $y$-axis.