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A new upward-convective short-wave instability mode in gas-sheared falling liquid films

Published online by Cambridge University Press:  02 December 2025

Misa Ishimura*
Affiliation:
Department of Mechanical Engineering, Yokohama National University , Kanagawa 240-8501, Japan
Sophie Mergui
Affiliation:
Sorbonne Université, CNRS, FAST, Université Paris-Saclay, Orsay 91405, France
Christian Ruyer-Quil
Affiliation:
CNRS, LOCIE, Université Savoie Mont Blanc, Le Bourget du Lac 73376, France
Georg Friedrich Dietze*
Affiliation:
Université Paris-Saclay, CNRS, FAST, Orsay 91405, France
*
Corresponding authors: Misa Ishimura, ishimura-misa-kx@ynu.ac.jp; Georg Friedrich Dietze, georg.dietze@cnrs.fr
Corresponding authors: Misa Ishimura, ishimura-misa-kx@ynu.ac.jp; Georg Friedrich Dietze, georg.dietze@cnrs.fr

Abstract

We investigate a short-wave instability mode recently identified via temporal stability analysis in weakly inclined falling liquid films sheared by a confined turbulent counter-current gas flow (Ishimura et al. J. Fluid Mech. vol. 971, 2023, p. A37). We perform spatio-temporal linear stability calculations based on the Navier–Stokes equations in the liquid film and the Reynolds-averaged Navier–Stokes equations in the gas, and compare these with our own experiments. We find that the short-wave instability mode is always upward-convective. The range of unstable group velocities is very wide and largely coincides with negative values of the wave velocity. Turbulence affects this mode both through the level of gas shear stress imparted and via the shape of the primary-flow gas velocity profile. Beyond a critical value of the counter-current gas flow rate, the short-wave mode merges with the long-wave Kapitza instability mode. The thus obtained merged mode is unstable for group velocities spanning from large negative to large positive values, i.e. it is absolute. The onset of the short-wave mode is precipitated by decreasing the channel height and inclination angle, and by increasing the liquid Reynolds number or the gas-to-liquid dynamic viscosity ratio. For vertically falling liquid films, merging occurs before the short-wave mode can become unstable on its own. Nonetheless, the ability to generate upward-travelling ripples is endowed to the merged mode. Preliminary calculations neglecting the linear perturbation of the turbulent viscosity suggest that three-dimensional perturbations could be more unstable than two-dimensional ones.

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JFM Papers
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Copyright
© The Author(s), 2025. Published by Cambridge University Press
Figure 0

Figure 1. Sketch of our experimental set-up. A falling liquid film of water flows down a glass plate inclined at an angle $\beta$ and, after transiting through a protected zone, enters in contact with a counter-current turbulent air flow within a rectangular channel of height $H^\star ={13}\,\textrm {mm}$ and width $W^\star ={270}\,\textrm {mm}$. The film surface deformation can be captured with two different cameras, a CCD camera with a line sensor (Basler, Sprint spl 4096) and a CMOS camera with a two-dimensional sensor (Basler, ace acA2440-75uc), both capturing a range of $x\approx {50}{-}{80}\,\textrm {cm}$. The photograph shows upward-travelling ripples emanating from the ISW mode.

Figure 1

Figure 2. Spatio-temporal shadowgraphs obtained from new experiments ($T\approx {22}\,^\circ\textrm{C}$) using the set-up of Ishimura et al. (2023). Falling water film sheared by a counter-current turbulent air flow: $H^\star ={13}\,\textrm {mm}$. Bright contours track spatio-temporal evolution of wave crests. (a–d) $\beta ={1}^\circ$, ${\textit{Re}}_{{L}}=103 \pm3$. (eh) $\beta ={5}^\circ$, ${\textit{Re}}_{{L}}=45.3 \pm1.1$. (a,e) Quiescent gas. (b,f) First evidence of the ISW mode. (c,g) Upward-travelling (in negative $x$-direction) ripples emanating from the ISW mode overpower Kapitza waves. (d,h) Ripples extend over the entire gas-sheared film surface. (b) ${\textit{Re}}_{{G}}=-2540$, (c) ${\textit{Re}}_{{G}}=-3040$, (d) ${\textit{Re}}_{{G}}=-3515$; ( f) ${\textit{Re}}_{{G}}=-5200$, (g) ${\textit{Re}}_{{G}}=-6620$, (h) ${\textit{Re}}_{{G}}=-6760$.

Figure 2

Figure 3. Experiments using CMOS camera with two-dimensional sensor ($T\approx {19.5}\,^\circ \textrm {C}$). Shadowgraphs showing upward-travelling ripples. Conditions similar to figures 2(c) and 2(d): $\beta =1^\circ$, $H^\star$ = 13 mm, ${\textit{Re}}_{{L}}=100\pm 3$. (a) ${\textit{Re}}_{{G}}=-3040$ (very close to ISW threshold); (b) ${\textit{Re}}_{{G}}=-3515$.

Figure 3

Figure 4. Frequency of upward-travelling ripples. Experiments with CCI probe for conditions according to figure 3(b). (a) Film thickness time trace obtained with 400 Hz acquisition frequency; (b) frequency spectrum obtained by averaging 20 film thickness time-trace signals of 25 s each. The frequency has been normalised with the linearly most-amplified frequency, $f^\star _{\textit{max}}={7.3}\,\textrm {Hz}$, obtained from a spatial linear stability calculation, and $\hat {h}_m$ denotes the amplitude of a Fourier mode with frequency $f^\star _m=m\Delta f^\star$, where $m\in \mathbb{Z}$ and $\Delta f^\star ={0.04}\,\textrm {Hz}$.

Figure 4

Figure 5. Falling liquid film (subscript ${L}$) on an inclined wall subject to a counter-current turbulent gas flow (subscript ${G}$). The flow is confined by an upper wall at $y^\star$ = $H^\star$ (not shown). In the linear limit, the gas flow is symmetrical about $y^\star$ = $D^\star$ = $(H^\star +h_0^\star )/2$. Magenta dashed lines illustrate the orthogonal curvilinear coordinate system used for the gas, ($\eta$, $\xi$), where $\eta$ = $\underline{y}d_0/d$. The subscript $0$ denotes the primary flow.

Figure 5

Figure 6. Primary-flow streamwise velocity profiles in the (a) liquid and (b) gas for $H^\star ={13}\,\textrm {mm}$, $\beta ={5}^\circ$, ${\textit{Re}}_{{L}}$ = 43.1, $T_{{{G}}0}^\star ={478}\,\textrm {N}\,\textrm {m}^{-2}$. Velocities are normalised with the respective maximum gas velocity. (a) Liquid-side velocity profiles; (b) gas-side velocity profiles at equivalent tangential gas shear stress. Solid line, solution for turbulent gas flow at ${\textit{Re}}_{{G}}=-1800$; dashed line, solution for laminar gas flow at ${\textit{Re}}_{{G}}=-4101$.

Figure 6

Figure 7. Spatio-temporal linear stability calculations for the conditions in figure 4(a) of Brevdo et al. (1999). Inclined falling liquid film in a passive atmosphere: ${\textit{Ka}}$ = 331.85, $\beta ={4.6}^\circ$, $\varPi _\rho$ = $\varPi _\mu$ = 0. (a) Saddle point (SP) curves. Upward triangles, $R$ = $(3/2){\textit{Re}}_{{L}}$ = 20; downward triangles, $R$ = 40; squares, $R$ = 60; diamonds, $R$ = 100; circles (branch I) and crosses (branch II), $R$ = 200. Dotted line segments correspond to unphysical SPs. (b–d) Collisions of spatial branches at the SPs marked by large coloured symbols in panel (a), $R$ = 200. Solid and dashed spatial branches move toward the corresponding SP as $\omega _i$ is decreased. (b) $V^\star _{\textit{ray}}/\mathcal{U}_{{Nu}}$ = 1.16, branch II: unphysical collision, $\omega ^\star _i\mathcal{T}_{{Nu}}$ = [0.02, 0.015, 0.01, 0.0079]; (c) $V^\star _{\textit{ray}}/\mathcal{U}_{{Nu}}$ = 1.16, branch I: physical collision, $\omega ^\star _i\mathcal{T}_{{Nu}}$ = [0.02, 0.015, 0.01, 0.0079, 0.0076]. Red dash-dotted line: ${\rm Im} \{\omega _k\}$ = 0; (d) $V^\star _{\textit{ray}}/\mathcal{U}_{{Nu}}$ = 1.23, $\omega ^\star _i\mathcal{T}_{{Nu}}$ = [0.0151, 0.0149, 0.0148, 0.014, 0.013, 0.0121]. Open circle, branch I, physical collision; cross, branch II, unphysical collision. Black solid and dotted lines, SP curves from panel (a).

Figure 7

Figure 8. Linear stability calculations for gas-sheared vertically falling liquid films. (a) Temporal calculations for the conditions in figure 4(e) of Schmidt et al. (2016): $H^\star ={10}\,\textrm {mm}$, ${\textit{Ka}}$ = 117.71, ${{\textit{Re}}_{{L}}}=6166$, ${\textit{Re}}_{{G}}$ = –48 322, $\delta _{{L}}$ = $h_0$ = $h_0$/$H^\star$ = 0.08, $\underline{Fr}= \underline{\mathcal{U}}/\sqrt {gH^\star }=3$, where $\underline{\mathcal{U}}$ = $[\partial _{x^\star }P_{{{G}} 0}^\star H^\star /\rho _{{G}}]^{1/2}$. Solid, numerical continuation with Auto07P; crosses, Chebyshev collocation approach (Ishimura et al.2023). (b) Spatial calculations for the conditions in figure 16 of Vellingiri et al. (2015): $H^\star ={30}\,\textrm {mm}$, ${\textit{Ka}}=1988.5$, $\underline{Re}$ = $gh_0^{\star 3}$/$\nu _{{L}}^2$ = 10, $\varTheta \in [0.1,2.5]$, with $\varTheta =T_{{G}}^\star /(\rho _{{L}} g^{2/3}\nu _{{L}}^{2/3})$.

Figure 8

Figure 9. Spatio-temporal stability calculations for the conditions in figure 8(b). SP curves ($\omega _k$ = 0) for selected values of $\varTheta$. Circles, $\varTheta$ = 1.0; upward triangles, $\varTheta$ = 1.21 (downward-CI/AI transition); diamonds, $\varTheta$ = 1.25; downward triangles, $\varTheta$ = 1.91 (AI/upward-CI transition); squares, $\varTheta$ = 2.5. (a) Temporal growth rate of perturbations persisting at long time; (b) wave speed. Filled symbols mark maximum $\omega _i$.

Figure 9

Table 1. Fluid properties used in our computations. The Kapitza number is ${{\textit{Ka}}}=\sigma /\rho _{{L}}/g^{1/3}/\nu _{{L}}^{4/3}$, where $g={9.81}\,\textrm {m}\,\textrm {s}^{-2}$ denotes the gravitational acceleration. Numbers between parentheses give the solvent mass fraction of aqueous solutions.

Figure 10

Figure 10. Temporal linear stability calculations. Parameters according to Ishimura et al. (2023): water/air (${\textit{Ka}}$ = 3174), $\beta ={5}^\circ$, $H^\star ={13}\,\textrm {mm}$, ${\textit{Re}}_{{L}}$ = 43.1. Thick solid blue with filled symbols, ISW mode; dashed black with open symbols, Kapitza mode; thin solid red with open symbols, unstable merged mode. Circles, ${\textit{Re}}_{{G}}$ = –4700; squares, ${\textit{Re}}_{{G}}$ = –5200; diamonds, ${\textit{Re}}_{{G}}$ = –5750; pentagons, ${\textit{Re}}_{{G}}$ = –6620. (a) Growth rate, $\omega _i$; (b) wave speed, $c_r$ = $\omega _r$/$k_r$.

Figure 11

Figure 11. SP curves obtained from spatio-temporal linear stability calculations. Parameters according to figure 10: water/air (${\textit{Ka}}$ = 3174), $\beta ={5}^\circ$, $H^\star ={13}\,\textrm {mm}$, ${\textit{Re}}_{{L}}$ = 43.1. Thick, physical SPs satisfying the Briggs collision criterion (Briggs 1964); thin dotted, unphysical SPs. Circles, ${\textit{Re}}_{{G}}$ = −4700; squares, ${\textit{Re}}_{{G}}$ = −5200; diamonds, ${\textit{Re}}_{{G}}$ = −5750; pentagons, ${\textit{Re}}_{{G}}$ = −6620. (a) ISW mode; (b) Kapitza mode. For ${\textit{Re}}_{{G}}$ = −5750 (diamonds) and ${\textit{Re}}_{{G}}$ = −6620 (pentagons), the Kapitza mode splits into three segments, two of which are represented here via dashed and dot-dashed curves. See figure 25 of Appendix C for all three segments.

Figure 12

Figure 12. Wave measures for the physical portions of the SP curves in figure 11 (thick lines there). Symbols mark the locus of SPs with maximum $\omega _i$. (a) Wave number; (b) wave speed in the laboratory reference frame; (c) imaginary part of the wave number, $k_i$, allowing to determine the spatial growth rate; (d) wave speed in the laboratory reference frame versus the wave number. Line styles and symbols as in figure 11.

Figure 13

Figure 13. Selected stability calculations for the ISW (solid blue) and Kapitza (dashed black) instability modes. Parameters according to figure 11(a) (squares there): ${\textit{Re}}_{{G}}$ = –5200. (a) SP curves, $\omega _k$ = 0. Thick, physical SPs; dotted, unphysical SPs. Symbols mark SPs used for checking Briggs collision criterion (Briggs 1964) in figure 14. (b) Temporal stability analysis for conditions in panel (a): $k_i$ = $V_{\textit{ray}}$ = 0. The maximum for $\omega _i$ is $\omega _i^{\textit{max}}$ = 15.1.

Figure 14

Figure 14. Verification of the Briggs collision criterion (Briggs 1964) for SPs marked by symbols in figure 13(a). Evolution of spatial branches (fixed $\omega _i$ and $V_{\textit{ray}}$) as $\omega _i$ is reduced from $\omega _i\gt \omega _i^{\textit{max}}$ (dash-dotted curves) to $\omega _i\lt \omega _i^{\textit{SP}}$ (dashed curves), where $\omega _i^{\textit{max}}=15.1$ is the maximum temporal growth rate observed in figure 13(b). The value of $\omega _i$ decreases from the dash-dotted line, via the dotted line, until the dashed line. (a) Physical SP on the ISW branch (filled square in figure 13a): $V_{\textit{ray}}$ = −57, $\omega _i^{\mathrm{\textit{SP}}}=6.96$, $\omega _i$ = $[15.3, 7.73, 6.01]$; (b) unphysical SP on the Kapitza branch (open square in figure 13a): $V_{\textit{ray}}$ = −44, $\omega _i^{\textit{SP}}=$−41.0, $\omega _i$ = [15.3, −39.5, −42.9]; (c) unphysical SP on the ISW branch (square with vertical division in figure 13a): $V_{\textit{ray}}$ = 63, $\omega _i^{\mathrm{\textit{SP}}}=0.882$, $\omega _i$ = $[15.3, 5.92, 0.687]$; (d) physical SP on the Kapitza branch (square with horizontal division in figure 13a): $V_{\textit{ray}}$ = 47, $\omega _i^{\mathrm{\textit{SP}}}=$−8.05, $\omega _i$ = [15.3, 3.78, −8.24].

Figure 15

Figure 15. Effect of the inclination angle, $\beta$, on the ISW (thick blue solid), Kapitza (thick black dashed and dash-dotted), and merged (thin red solid) instability modes. Parameters according to figure 11. Spatio-temporal stability formulation: $\omega _k$ = 0. Dotted (blue, black and red) lines correspond to unphysical SPs, where the Briggs collision criterion is not satisfied. (a) $\beta$ = ${5}^\circ$. Circles, ${\textit{Re}}_{{G}}$ = −4700; diamonds, ${\textit{Re}}_{{G}}$ = −5750; pentagons, ${\textit{Re}}_{{G}}$ = −6620. (b) $\beta$ = ${10}^\circ$. Circles, ${\textit{Re}}_{{G}}$ = −6000; diamonds, ${\textit{Re}}_{{G}}$ = −6600; pentagons, ${\textit{Re}}_{{G}}$ = −8000. (c) $\beta$ = ${15}^\circ$. Circles, ${\textit{Re}}_{{G}}$ = −7135; diamonds, ${\textit{Re}}_{{G}}$ = –7600; pentagons, ${\textit{Re}}_{{G}}$ = −8500. For ${\textit{Re}}_{{G}}$ = −8500, there are no physical instability modes for $V_{\textit{ray}}\gt 12.5$. (d) $\beta$ = ${90}^\circ$. Circles, ${\textit{Re}}_{{G}}$ = −5000; diamonds, ${\textit{Re}}_{{G}}$ = −9000; pentagons, ${\textit{Re}}_{{G}}$ = −12 000.

Figure 16

Figure 16. Role of turbulence in shaping the ISW, Kapitza and merged instability modes. Parameters according to figures 15(a) and 15(d). Comparison of SP curves for turbulent (curves with regular symbols) and laminar (curves with large symbols, $\tilde {l}_{\mathrm{t}}$ = 0 in (3.11g)) primary-flow gas velocity profiles at equivalent $T^\star _{{{G}} 0}$. (a) $\beta$ = ${5}^\circ$, $T^\star _{{{G}} 0}={3170}\,\textrm {N} \,\textrm {m}^{-2}$ (figure 15a). Regular diamonds, ${\textit{Re}}_{{G}}$ = −5750; large diamond, ${\textit{Re}}_{{G}}$ = −26 233. (b) $\beta$ = ${90}^\circ$, $T^\star _{{{G}} 0}=10\,100 \,\textrm {N} \, \textrm {m}^{-2}$ (figure 15d). Regular pentagons, ${\textit{Re}}_{{G}}$ = −12 000; large pentagons, ${\textit{Re}}_{{G}}$ = −90 712.

Figure 17

Figure 17. Role of the linear gas stress perturbations, $\check {T}_{{G}}$ and $\check {P}_{{G}}$, defined in (3.23), in shaping the ISW and Kapitza modes via (3.7d) and (3.7e). Saddle-point curves for one set of parameters from figure 11: ${\textit{Re}}_{{G}}$ = −5200. Solid lines with squares, full model; dashed with crosses, $\hat {T}_{{G}}$ = 0 in (3.7d); dash-dotted with asterisks: $\hat {P}_{{G}}$ = 0 in (3.7e). (a) ISW mode; (b) Kapitza mode.

Figure 18

Figure 18. Physical portions of the SP curves from figures 15(a) and 15(b) replotted in the $\omega _i$ versus $k_r$ plane. Crosses mark neutral points ($\omega _i$ = 0) obtained from corresponding temporal stability calculations ($k_i$ = $V_{\textit{ray}}$ = 0). (a) $\beta ={5}^\circ$ (figure 15a). Circles, ${\textit{Re}}_{{G}}$ = −4700; asterisks, ${\textit{Re}}_{{G}}$ = −4915; squares, ${\textit{Re}}_{{G}}$ = −5200; diamonds, ${\textit{Re}}_{{G}}$ = −5750; pentagons, ${\textit{Re}}_{{G}}$ = −6620. (b) $\beta ={10}^\circ$ (figure 15b). Circles, ${\textit{Re}}_{{G}}$ = −6000; diamonds, ${\textit{Re}}_{{G}}$ = −6600; pentagon, ${\textit{Re}}_{{G}}$ = −8000.

Figure 19

Figure 19. Effect of the channel height, $H^\star$, on the ISW mode. Parameters based on figure 11: $\beta$ = 5$^\circ$, ${\textit{Re}}_{{L}}$ = 43.1. (a) Neutral point curves ($\omega _i$ = 0) from temporal formulation associated with the ISW (thick solid), Kapitza (dashed) and merged (thin solid) instability modes: ${\textit{Ka}}$ = 3174 (water/air). Filled symbols, instability threshold of the ISW mode; open symbols, merging point (MP); crosses, flooding point (FP). From circles to triangles, $H^\star$ = $[13,19,25,35,50]$ mm. Asterisks, spatio-temporal calculation. Thin cyan curve with plus sign tracks ISW neutral bound. (b) ISW neutral bound in terms of $H/h_0$ versus ${\textit{Re}}_{{G}}$ for different liquids from table 1 in contact with air. From crosses to pentagons, ${\textit{Ka}}$ = $[17.78,121.4,509.5,963.2,301.3,3174,1988]$, $\varPi _\mu$ = $[0.0009,0.004,0.0058,0.0078,0.0076,0.018,0.031]$.

Figure 20

Figure 20. Effect of the liquid Reynolds number, ${\textit{Re}}_{{L}}$, on the onset of the ISW mode. Neutral point curves for two fluid combinations from table 1: $H^\star ={13}\,\textrm {mm}$, $\beta ={5}^\circ$. From pentagons to triangles, ${\textit{Re}}_{{L}}$ = $[5,10,20,43.1,80]$. (a) ${\textit{Ka}}$ = 3174 (water/air); (b) ${\textit{Ka}}$ = 17.78 (silicone oil II/air).

Figure 21

Figure 21. Effect of the inclination angle, $\beta$, on the onset of the ISW mode. Parameters based on figure 11: water/air, $H^\star ={13}\,\textrm {mm}$. (a) Neutral point curves for different values of $\beta$: ${\textit{Ka}}$ = 3174, ${\textit{Re}}_{{L}}$ = 43.1. From circle to pentagon, $\beta$ = $[5,10,15,90]^\circ$. (b) ISW neutral bound in terms of $\beta$ versus ${\textit{Re}}_{{G}}$ for different values of ${\textit{Re}}_{{L}}$: ${\textit{Ka}}$ = 3510. Solid curves with filled symbols, linear stability calculations. Filled symbols mark (physical or numerical) end of ISW LP tracking. Downward triangle, ${\textit{Re}}_{{L}}$ = 10; pentagon, ${\textit{Re}}_{{L}}$ = 20.5; upward triangle, ${\textit{Re}}_{{L}}$ = 43.1; diamond, ${\textit{Re}}_{{L}}$ = 46; square, ${\textit{Re}}_{{L}}$ = 103; circle, ${\textit{Re}}_{{L}}$ = 167.5. Open symbols, ISW threshold obtained from our experiments (§ 2). Pentagon, ${\textit{Re}}_{{L}}$ = 20.5; diamonds, ${\textit{Re}}_{{L}}\in [44,48]$; squares, ${\textit{Re}}_{{L}}$ = 103; circles, ${\textit{Re}}_{{L}}\in [167,168]$. (c) Neutral wave speed corresponding to panel (a). (d) Neutral angular frequency corresponding to panel (a).

Figure 22

Figure 22. Comparison of the ISW and AI thresholds for parameters according to figures 19(b) and 21(b). Dashed curves with open symbols, AI threshold ($\omega _i$ = $V_{\textit{ray}}$ = 0); solid lines with filled symbols, ISW threshold. (a) Effect of the channel height, $H^\star$, for parameters from figure 19(b). From diamonds to pentagons, ${\textit{Ka}}$ = $[121.4,3174,1988]$, $\varPi _\mu$ = $[0.004,0.018,0.031]$. (b) Effect of the inclination angle, $\beta$, for parameters from figure 21(b). Magenta triangles, ${\textit{Re}}_{{L}}$ = 43.1; blue squares, ${\textit{Re}}_{{L}}$ = 103.

Figure 23

Figure 23. Three-dimensional (3-D) temporal ($\breve {k}_i$ = 0) stability calculations for the conditions in figures 10(a) and 19(a): water/air (${\textit{Ka}}$ = 3174), $\beta ={5}^\circ$, $H^\star ={13}\,\textrm {mm}$, ${\textit{Re}}_{{L}}$ = 43.1. 3-D calculations are based on our equivalent two-dimensional formulation via (A10). (a) Validation with two-dimensional (2-D) calculations based on (3.7) and (3.21): ${\textit{Re}}_{{G}}$ = -6620. Solid red, 2-D calculation from figure 10(a), where $S^t_{11}=S^t_{22}=0$ and $\mu _t$ according to (3.11g); dashed, 2-D calculation with $\mu _t$ according to (A4c); dash-dotted, 2-D calculation with $S^t_{11},S^t_{22}{\ne }0$ and $\mu _t$ according to (A4c);, magenta thin solid, 2-D calculation with $S^t_{11},S^t_{22}{\ne }0$, $\mu _t$ according to (A4c) and $\check {\mu }_t$ = 0; magenta open pentagons, 3-D calculation with $k_z$/$k_x$ = 0. (b) Neutral point curves for different values of $k_z$/$k_x$. Circles, $k_z$/$k_x$ = 0; crosses, $k_z$/$k_x$ = 0.4; diamonds, $k_z$/$k_x$ = 0.8; pentagons, $k_z$/$k_x$ = 2; squares, $k_z$/$k_x$ = 3.

Figure 24

Figure 24. Temporal linear stability calculations obtained via numerical continuation (black solid) and Chebyshev collocation (coloured dashed lines with symbols). Conditions from figure 8(b) according to Vellingiri et al. (2015): ${{\textit{Ka}}}=1988.5$, ${{\textit{Re}}}=gh_0^{\star 3}/\nu _{{L}}^2=10$, $H^\star ={30}\,\textrm {mm}$, $\varTheta =T_{{G}}^\star /(\rho _{{L}} g^{2/3}\nu _{{L}}^{2/3})$. (a,d) Dispersion curves; (b,e) liquid-side eigenfunction; (c,f) gas-side eigenfunction. (a,b,c) $\varTheta$ = 1.21 (downward-CI/AI transition). Circles, $N_{{p}}$ = 10; squares, $N_{{p}}$ = 30; diamonds, $N_{{p}}$ = 80; pentagons, $N_{{p}}$ = 160. (d,e,f) $\varTheta$ = 1.91 (AI/upward-CI transition). Circles, $N_{{p}}$ = 10; squares, $N_{{p}}$ = 30; diamonds, $N_{{p}}$ = 100; pentagons, $N_{{p}}$ = 160.

Figure 25

Figure 25. All SP curves for the parameters in figure 11. Line styles as in figure 11. New green lines with open symbols and thick solid segments (corresponding to physical SPs satisfying Briggs collision criterion): additional Kapitza modes, bridging a small gap in $V_{\textit{ray}}$ not covered by the SP curves in figure 11(b). Diamonds, ${\textit{Re}}_{{G}}=-5750$; pentagons, ${\textit{Re}}_{{G}}=-6620$. Crosses indicate loss of SPs in the limit $k_r{\to }0$. (a) SP curves corresponding to the Kapitza mode. (b) Physical portions of all SP curves corresponding to the ISW and Kapitza modes.