 Open Access Article
 Open Access Article
      
        
          
            Ludovic 
            Keiser
          
        
       ab, 
      
        
          
            Loukas 
            Stamoulis
ab, 
      
        
          
            Loukas 
            Stamoulis
          
        
       a, 
      
        
          
            Baptiste 
            Georjon
          
        
      a, 
      
        
          
            Philippe 
            Marmottant
a, 
      
        
          
            Baptiste 
            Georjon
          
        
      a, 
      
        
          
            Philippe 
            Marmottant
          
        
       a and 
      
        
          
            Benjamin 
            Dollet
a and 
      
        
          
            Benjamin 
            Dollet
          
        
       *a
*a
      
aUniv. Grenoble Alpes, CNRS, LIPhy, 38000 Grenoble, France. E-mail: benjamin.dollet@univ-grenoble-alpes.fr
      
bUniversité Côte d'Azur, CNRS, Institut de Physique de Nice, UMR 7010, 06200 Nice, France
    
First published on 19th August 2025
Controlling the removal of bubbles from channels is crucial in microfluidics, either to eliminate air pockets if they are unwanted, or in pumpless microfluidic applications where receding bubbles is a way to induce liquid flows. To provide a better physical understanding of air removal in microchannels, we study the dynamics of invasion of wetting liquids in dead-end microchannels surrounded by an air-permeable medium. Using polydimethylsiloxane (PDMS)-based devices, we demonstrate that gas permeation through the channel walls drives an exponential decay in trapped air length with time (in marked contrast with the so-called Lucas–Washburn law of imbibition in porous media), providing a straightforward route to bubble elimination. Systematic experiments varying channel width, height, and PDMS thickness reveal how geometric and material factors modulate the refilling timescale. A simple analytical model, coupling capillarity and gas diffusion, captures these results quantitatively. For this purpose, we introduce an explicit expression for the interfacial curvature in microchannels with heterogeneous wettability (e.g., PDMS-on-glass). This framework offers practical guidelines for microfluidic engineers aiming to prevent or remove trapped bubbles without relying on active pumping.
Microfluidic systems present additional motivations for studying liquid imbibition, particularly when undesired air bubbles enter a chip. Such bubbles can result from incomplete priming, dissolved gas emerging under pressure/temperature shifts, or imperfect sealing of the microchannel network. Once formed, they can severely disrupt flow patterns, obstruct the transport of important reagents or cells, and even cause oxidative or chemical reactions if retained in oxygen-sensitive processes. Consequently, there is strong incentive to eliminate these trapped air pockets, which connects directly to the idea of liquid imbibition removing gas from otherwise inaccessible parts of the device.
Kang et al.8 studied the elimination of spurious bubbles in microfluidic channels, by permeation through PDMS walls under pressurisation. Their experiments revealed an exponential decay in bubble volume, which is faster when the overpressure in the channels increases. Another strategy to eliminate bubbles in microchannels has been proposed by Guo et al.,9 using three parallel channels separated by constrictions. Interestingly, they mention that their device is bioinspired by the repair of embolisms in angiosperms,7,10–12 although this biological question is still hotly debated and that the possible repair mechanisms in plants remain unclear. They recover an exponential decay of the bubbles, and show experimentally that the decay time increases with the channel width and the PDMS thickness.
Xu et al.13 provided a broader review of air transport through PDMS for applications, mentioning that air can be eliminated from the channels either by first degassing the PDMS itself, or by applying a low-pressure environment in separate, adjacent chambers, thus drawing the gas out from the channels of interest. Not only can this be used to eliminate air bubbles, but it opens the way to vacuum-driven power-free pumpless microfluidics, with applications e.g. for blood separation or cell cultures. This possibility to operate microfluidic devices for sample preparation without complicated and bulky pumping has developed recently a lot of interest.14–18 A comprehensive overview of pervaporation-based strategies and other mass-transfer-driven microfluidics has also been provided by Bacchin et al.19
However, the dynamics of liquid refilling (or bubble removal) in PDMS microchannels has hitherto not been rationalised by a comprehensive model, whilst it is necessary to control the timescale associated to e.g. pumpless microfluidics. In particular, the dynamics is often quantified in terms of permeability through a thin membrane of thickness δ.8,9,13 However, in most practical situations in microfluidics, the PDMS surrounding the channels cannot be identified to a thin membrane, because of side effects (fluxes from the side walls of the channel) and because the top PDMS part of the channel must generally not be too compliant. To account for these complications (as compared to the simple membrane case), empirical correction factors have been proposed,8 but they have not been related to the device geometry by a predictive model. This calls for a proper study of the influence of all geometrical parameters: not only PDMS thickness, but also channel width and height, on the flux.
In this paper, we revisit the problem of bubble removal and liquid imbibition in PDMS microchannels, focusing on dead-end geometries in which air cannot be simply swept away by a primary flow. We present experiments under well-controlled capillary overpressure conditions, systematically varying channel width, height, and PDMS thickness. We then propose a theoretical framework that accounts for both capillary and imposed pressures, combined with mass transport through the entire PDMS bulk. This allows us to quantify precisely the timescale of bubble shrinkage and channel refilling, moving beyond the previously reported exponential fitting. Our objective is to provide microfluidic users with a simple, yet robust predictive tool for controlling bubble dynamics in permeable environments, thereby improving the reliability of pumpless microfluidic technologies and other air-permeable-medium-based applications.
The polydimethylsiloxane, a silicone elastomer hereafter referred to as PDMS, (Sylgard™ 184, Dow) is prepared by thoroughly mixing a 10![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) :
:![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) 1 mass ratio of base to curing agent. The mixture undergoes vacuum degassing for approximately one hour to eliminate trapped air. A controlled volume (e.g., 2.5 mL) of this degassed solution is then spread over the structured wafer by spin coating for 10 s at 500 rpm, followed by 40 s at speeds between 700 and 2000 rpm, depending on the desired PDMS thickness H. The coated wafer is then placed for an additional hour to ensure uniform levelling of the film, before the curing step.
1 mass ratio of base to curing agent. The mixture undergoes vacuum degassing for approximately one hour to eliminate trapped air. A controlled volume (e.g., 2.5 mL) of this degassed solution is then spread over the structured wafer by spin coating for 10 s at 500 rpm, followed by 40 s at speeds between 700 and 2000 rpm, depending on the desired PDMS thickness H. The coated wafer is then placed for an additional hour to ensure uniform levelling of the film, before the curing step.
The spin-coated PDMS is then cured in an oven at 65 °C for 24 h. Once polymerised, the flexible PDMS layer is gently released from the silicon wafer, exposing the channel features in negative topography. A brief atmospheric plasma treatment on a glass slide provides a surface amenable to bonding. Finally, the PDMS is carefully placed onto the plasma-treated slide.
Since we wanted to avoid the potential complications associated with solutions, this early observation led us to search for pure liquids that present good wetting with PDMS, hence liquids of low surface tension. The wetting liquid should be not too soluble in PDMS to minimise swelling.25 Lastly, it must be not too volatile, to keep a little reservoir of liquid at the entrance of the channel throughout the experiments. The alcohol family presents some good candidates, and we chose pentan-1-ol (henceforth called pentanol for simplicity) to produce all of the experimental data and results presented in this work, except in sec. 3.4 where a comparison with octanol is made. We note for future reference that the contact angle of pentanol on PDMS is around θ = 30°.26
![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) | = −dL/dt which itself decreases with time. The dynamics is faster for narrower channels.
| = −dL/dt which itself decreases with time. The dynamics is faster for narrower channels.
        The experimental dynamics is extremely well fitted by an exponential decay:
| L(t) = L(t = 0)e−t/τ, | (1) | 
To confirm the validity of the exponential decay, we also extract the rate of decrease |![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) | by finite differences on the experimental data of L(t), and plot it as a function of L, in the inset of Fig. 3a. Although the data are more noisy, as always when estimating a time derivative of discrete data, they agree very well with a linear law of the form |
| by finite differences on the experimental data of L(t), and plot it as a function of L, in the inset of Fig. 3a. Although the data are more noisy, as always when estimating a time derivative of discrete data, they agree very well with a linear law of the form |![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) | = L/τL. Moreover, the values of τL measured as the best fitting slope in the inset of Fig. 3a agree with the value of τ measured as the best fitting parameter in Fig. 3a within 3%.
| = L/τL. Moreover, the values of τL measured as the best fitting slope in the inset of Fig. 3a agree with the value of τ measured as the best fitting parameter in Fig. 3a within 3%.
To assess the robustness and reproducibility of our results, we recorded five independent time evolutions L(t) in a channel with a given geometry in Fig. 3b. The corresponding five curves all collapse together, and they are all extremely well fitted by the exponential law (1). From the statistics of the five fitted timescales τ, we get τ = 47.0 ± 0.7 s: the very small value of the standard deviation compared to the mean confirms the reproducibility of our measurements.
|  | ||
| Fig. 5 (a) Plot of the imbibition timescale as a function of the channel length, for channels of dimensions h = 60 μm, H = 116.5 μm, and w = 60 (○), 80 (□), 100 (◊), 120 (△) and 140 μm (▽). Lines are average of the data; the statistics over each series of four data points gives: T = 525 ± 4, 714 ± 4, 861 ± 7, 1000 ± 15 and 1105 ± 28 s respectively for w = 60, 80, 100, 120 and 140 μm. (b) Plot of the imbibition timescale as a function of the channel width, for channels of dimensions h = 60 μm, L0 = 18 mm, and δ = 57 (◊) and 127 μm (△). The linear size of the symbols is proportional to the channel width. The curves are fits by (11), where a = (DS∞airγ)−1 is taken as a free fitting parameter, with value a = 0.0258 and 0.0231 μm−3 s respectively for δ = 57 and 127 μm. (c) Plot of the imbibition timescale as a function of the channel height, for fixed channel length L0 = 18 mm and width w = 100 μm, and fixed upper wall thickness δ = 57.9 ± 1.8 μm. The curve is a fit by (11), where a = (DS∞airγ)−1 is taken as a free fitting parameter, with value a = 0.0259 μm−3 s. For (a), (b) and (c), the chosen values of the parameters (L0, w, h and δ) were selected to enable the independent variation of each geometric factor, ensuring that their individual influence on the imbibition timescale could be clearly assessed. | ||
Next, we plot the imbibition timescale as a function of the channel width, for two different upper wall thicknesses, at fixed channel length and height, in Fig. 5b. It evidences the increase of the imbibition timescale at increasing width, with a slight concave trend.
Finally, we plot the imbibition timescale as a function of the channel height, at fixed channel width and length and fixed upper wall thickness, in Fig. 5c. It is much more difficult to obtain these data points, because each channel height requires making a new mold, and because aiming at a constant upper wall thickness requires to adjust the spin coating velocity of PDMS with some trial and error (whence the error bar on δ mentioned in the caption of Fig. 5c, which comes from the statistical dispersion of the three measured values of δ). For this reason, we could obtain only three data points in Fig. 5c. However, they are noteworthy because they show that the imbibition timescale increases strongly, and in a superlinear fashion, with the channel height.
|  | ||
| Fig. 6 Time evolution of the length of the air pocket, for four channels with dimensions L0 = 18 mm, h = 60 μm, H = 180 μm, and w = 80 (blue), 100 (green), 120 (violet) and 140 μm (red). The channels were filled with pentanol (○) and octanol (▷). The lines (simple for pentanol, dotted for octanol) are fits by eqn (1). Inset: ratio of the imbibition timescales of pentanol τpent and octanol τoct, as a function of channel width. | ||
Since pentanol is wetting the channel walls, Laplace pressure implies that the air pocket inside the channel is in overpressure relative to the liquid in contact with the meniscus, the pressure difference being equal to γ![[capital script C]](https://www.rsc.org/images/entities/char_e522.gif) with γ the surface tension and
 with γ the surface tension and ![[capital script C]](https://www.rsc.org/images/entities/char_e522.gif) the curvature of the meniscus. Assuming that pressure variations are negligible in the liquid, an assumption that we will shortly justify, the air trapped in the channel is therefore in overpressure relative to the ambient air around the channel. Hence, the air bubble tends to permeate outwards, which justifies the decrease of L.
 the curvature of the meniscus. Assuming that pressure variations are negligible in the liquid, an assumption that we will shortly justify, the air trapped in the channel is therefore in overpressure relative to the ambient air around the channel. Hence, the air bubble tends to permeate outwards, which justifies the decrease of L.
| hw ![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) = −Q, | (2) | 
|  | (3) | 
The next step consists in predicting q. This permeation rate per unit length arises from the outwards diffusion of air within the PDMS resulting from the pressure difference between the air pocket and the atmosphere; using Fick's law, we have:
| q = −∫D∇c·nds, | (4) | 
![[small script l]](https://www.rsc.org/images/entities/i_char_e146.gif) ≈ 10−4 m, the typical diffusion time in the cross-section is
 ≈ 10−4 m, the typical diffusion time in the cross-section is ![[small script l]](https://www.rsc.org/images/entities/i_char_e146.gif) 2/D ≈ 3 s, which is two orders of magnitude smaller than the measured values of τ in almost all experiments (see sec. 3.3), except for the smallest channel heights. Hence, we may consider that the diffusion is quasisteady, and the concentration field obeys the two-dimensional Laplace equation in the cross-section.
2/D ≈ 3 s, which is two orders of magnitude smaller than the measured values of τ in almost all experiments (see sec. 3.3), except for the smallest channel heights. Hence, we may consider that the diffusion is quasisteady, and the concentration field obeys the two-dimensional Laplace equation in the cross-section.
        To get the boundary conditions, it is required to know the amount of dissolved air in the PDMS in the range of pressures of the experiments. For this, we use the solubility coefficient ![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) ,27 defined such that c =
,27 defined such that c = ![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) p at the PDMS/gas boundaries, where p is the partial pressure of air. This linear relationship is an example of Henry's law, and it is valid because the air concentration in PDMS is small. Hence, we take the following boundary conditions: at the PDMS/atmosphere interface, c =
p at the PDMS/gas boundaries, where p is the partial pressure of air. This linear relationship is an example of Henry's law, and it is valid because the air concentration in PDMS is small. Hence, we take the following boundary conditions: at the PDMS/atmosphere interface, c = ![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) patm, with patm = 1 atm = 105 Pa, and at the PDMS/channel interface, c =
patm, with patm = 1 atm = 105 Pa, and at the PDMS/channel interface, c = ![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) pin, with pin the pressure inside the gas pocket, neglecting the influence of the pentanol vapour in the gas pocket. Finally, there is no flux at the glass/PDMS interface.
pin, with pin the pressure inside the gas pocket, neglecting the influence of the pentanol vapour in the gas pocket. Finally, there is no flux at the glass/PDMS interface.
Let us define the following dimensionless function related to the concentration field:
|  | (5) | 
|  | (6) | 
| f = 1 at y = h and |x| ≤ w/2, and at |x| = w/2 and 0 ≤ y ≤ h. | 
The second of these three conditions expresses that glass is impermeable to air. This problem has been solved analytically in Appendix A of ref. 21. In particular, as long as δ/w ≤ 1.5 or h/w ≤ 0.1, a condition met in our experiments, the following approximation was found to hold within 1%:
|  | (7) | 
Coming back to the definition (5) of f and plugging (7) into (4), we thus get the flux:
|  | (8) | 
![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) ) + (p
) + (p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) − patm), where p
 − patm), where p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) in the pressure in the liquid in contact with the meniscus. Hence, pin − p
 in the pressure in the liquid in contact with the meniscus. Hence, pin − p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) is the Laplace pressure across the meniscus. A difficulty in our experiments is that the meniscus is in contact with two different materials: PDMS at the side walls and at the top wall, and glass at the bottom wall. Since glass is more hydrophilic than PDMS, the contact angle of pentanol on glass θ′ is lower than the contact angle θ = 30° of pentanol on PDMS. To account for this presence of two different materials, which is an ubiquitous situation in microfluidics owing to the frequent gluing of PDMS channels on glass slides, the following expression of the capillary pressure has been claimed to apply without justification28 and quoted in subsequent review articles:29pin − p
 is the Laplace pressure across the meniscus. A difficulty in our experiments is that the meniscus is in contact with two different materials: PDMS at the side walls and at the top wall, and glass at the bottom wall. Since glass is more hydrophilic than PDMS, the contact angle of pentanol on glass θ′ is lower than the contact angle θ = 30° of pentanol on PDMS. To account for this presence of two different materials, which is an ubiquitous situation in microfluidics owing to the frequent gluing of PDMS channels on glass slides, the following expression of the capillary pressure has been claimed to apply without justification28 and quoted in subsequent review articles:29pin − p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) = γ[(cos
 = γ[(cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ + cos
θ + cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ′)/h + 2
θ′)/h + 2![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) cos
cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ/w]. However, this unjustified formula is erroneous, and we derive in the Appendix the correct formula for arbitrary, extending a method introduced by Mason and Morrow.30 Taking for simplicity θ′ = 0, hence assuming that pentanol is perfectly wetting on glass, this formula reads:
θ/w]. However, this unjustified formula is erroneous, and we derive in the Appendix the correct formula for arbitrary, extending a method introduced by Mason and Morrow.30 Taking for simplicity θ′ = 0, hence assuming that pentanol is perfectly wetting on glass, this formula reads:|  | (9) | 
![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) is γ/h ≈ 3 × 102 Pa.
 is γ/h ≈ 3 × 102 Pa.
        We now argue that |p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) – patm| ≪ pin − p
 – patm| ≪ pin − p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) . Three terms may contribute to p
. Three terms may contribute to p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) – patm: the Laplace pressure at the surface of the drop, a gravitational term over the height of the drop, and a viscous pressure drop in the liquid set into motion by the bubble shrinkage. In our experiments, the drop is flat and Laplace pressure is certainly orders of magnitude lower than at the meniscus between the bubble and the liquid (Fig. 1 is not at scale). The height of the drop is less than 1 mm, hence hydrostatic pressure remains lower than 10 Pa. To estimate the viscous pressure drop, we assume that a length L0 − L of the liquid in the channel is entrained at the velocity of the meniscus |
 – patm: the Laplace pressure at the surface of the drop, a gravitational term over the height of the drop, and a viscous pressure drop in the liquid set into motion by the bubble shrinkage. In our experiments, the drop is flat and Laplace pressure is certainly orders of magnitude lower than at the meniscus between the bubble and the liquid (Fig. 1 is not at scale). The height of the drop is less than 1 mm, hence hydrostatic pressure remains lower than 10 Pa. To estimate the viscous pressure drop, we assume that a length L0 − L of the liquid in the channel is entrained at the velocity of the meniscus |![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) | (hence we neglect pervaporation effects), and we use Poiseuille law in a rectangular channel: |
| (hence we neglect pervaporation effects), and we use Poiseuille law in a rectangular channel: |![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) | =
| = ![[scr S, script letter S]](https://www.rsc.org/images/entities/char_e532.gif) ∇p/η, with ∇p the pressure gradient, η = 4 × 10−3 Pa s the liquid viscosity and an effective section given by (see e.g.31):
∇p/η, with ∇p the pressure gradient, η = 4 × 10−3 Pa s the liquid viscosity and an effective section given by (see e.g.31):
![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) |/h2. With the exponential law L(t) = L0e−t/τ, the quantity (L0 − L)|
|/h2. With the exponential law L(t) = L0e−t/τ, the quantity (L0 − L)|![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) | has as upper bound L20/(4τ). Hence, the viscous pressure drop is lower than 3ηL20/(h2τ). This quantity is equal to 2 Pa with L0 = 18 mm, h = 60 μm and τ = 5 × 102 s (an order of magnitude given by Fig. 5b). This remains more than two orders of magnitude lower than Laplace pressure (9). Altogether, the pressure variations within the liquid remain negligible with Laplace pressure (9), which we can therefore identify to the term pin − patm in (8). Therefore, we get the final prediction
| has as upper bound L20/(4τ). Hence, the viscous pressure drop is lower than 3ηL20/(h2τ). This quantity is equal to 2 Pa with L0 = 18 mm, h = 60 μm and τ = 5 × 102 s (an order of magnitude given by Fig. 5b). This remains more than two orders of magnitude lower than Laplace pressure (9). Altogether, the pressure variations within the liquid remain negligible with Laplace pressure (9), which we can therefore identify to the term pin − patm in (8). Therefore, we get the final prediction|  | (10) | 
Inserting this expression in (3), we predict the imbibition time:
|  | (11) | 
![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) γ)−1 taken as a fitting parameter. These fits show that the model captures qualitatively all the trends, namely the increase of the imbibition timescale at increasing width, increasing upper wall thickness and increasing channel height. In particular, it reproduces excellently the dependence on the channel height (Fig. 5c), whilst it predicts slightly stronger variations with the channel width than the measurements (Fig. 5b). We also notice that the obtained values of the fitting parameter a, taken independently for each series of data, are consistent within 7%; averaging them yields a = 0.0240 ± 0.0016 μm−3 s. This suggests that our model includes the essential ingredients to understand the role of the geometrical parameters on the imbibition dynamics.
γ)−1 taken as a fitting parameter. These fits show that the model captures qualitatively all the trends, namely the increase of the imbibition timescale at increasing width, increasing upper wall thickness and increasing channel height. In particular, it reproduces excellently the dependence on the channel height (Fig. 5c), whilst it predicts slightly stronger variations with the channel width than the measurements (Fig. 5b). We also notice that the obtained values of the fitting parameter a, taken independently for each series of data, are consistent within 7%; averaging them yields a = 0.0240 ± 0.0016 μm−3 s. This suggests that our model includes the essential ingredients to understand the role of the geometrical parameters on the imbibition dynamics.
      We can also test the predictions for different liquids, here pentanol and octanol (Fig. 6). According to (11), at given channel geometry, the ratio of the imbibition times of the two liquids should be constant and equal to the inverse ratio of their surface tensions: τpent/τoct = γoct/γpent at given contact angle θ. The imbibition timescale ratio was found to be almost constant in experiments (see inset in Fig. 6). Using the values γpent = 25.4 mN m−1, γoct = 27.1 mN m−1, given for T = 25 °C in,33 and comparing with the values obtained from curve fitting, we find that the results are predicted well by the theory: we get τpent/τoct = 1.03 whilst γoct/γpent = 1.07. The remaining small discrepancy likely comes from a difference of contact angle between pentanol and octanol on PDMS.
We now discuss the value of the fitting parameter a. To have a numerical value for the solubility, we use the data of Merkel et al.,27 who measured the solubility S of various gases in PDMS. Merkel et al. showed that the solubility is well represented by an affine law S = S∞ (1 + np), and provide the following values (see Tab. II in27) for N2:  and nN2 = 3 × 10−3 atm−1, and for O2:
 and nN2 = 3 × 10−3 atm−1, and for O2:  and nO2 = 5 × 10−3 atm−1. Since our pressures remain of order 1 atm = 105 Pa, these numerical data show that we may take S = S∞ as a good approximation. In the value of the solubility, 1 cm3STP is the number of moles that would occupy one cubic centimeter at standard temperature and pressure, as calculated via the ideal gas law. In our model, since c is dimensionless, we use the following unit conversion:
 and nO2 = 5 × 10−3 atm−1. Since our pressures remain of order 1 atm = 105 Pa, these numerical data show that we may take S = S∞ as a good approximation. In the value of the solubility, 1 cm3STP is the number of moles that would occupy one cubic centimeter at standard temperature and pressure, as calculated via the ideal gas law. In our model, since c is dimensionless, we use the following unit conversion: ![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) = 1 cm3STP cm−3 atm−1 corresponds to
 = 1 cm3STP cm−3 atm−1 corresponds to ![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) = 1 atm−1 = 10−5 Pa−1. Hence, if we consider a simplified atmosphere composed of 79% of O2 and of 21% of N2, we take the linear combination of the contributions of these two gases (which is justified by the additivity of the partial pressures), whence the following value of the air solubility:
 = 1 atm−1 = 10−5 Pa−1. Hence, if we consider a simplified atmosphere composed of 79% of O2 and of 21% of N2, we take the linear combination of the contributions of these two gases (which is justified by the additivity of the partial pressures), whence the following value of the air solubility:  . Hence, we shall use
. Hence, we shall use ![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) = 1.1 × 10−6 Pa−1. With the values already mentioned: D = 3.4 × 10−9 m2 s−1 and γ = 25 mN m−1, this gives (D
 = 1.1 × 10−6 Pa−1. With the values already mentioned: D = 3.4 × 10−9 m2 s−1 and γ = 25 mN m−1, this gives (D![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) γ)−1 = 0.0105 μm−3 s. This value agrees in order of magnitude with our fitting value a = 0.024 μm−3 s, but it is two times lower. We shall discuss later some reasons for this discrepancy, in relation with some simplifying assumptions of the model. However, a probable explanation for this factor-of-two difference is the specific PDMS recipe used here, which differs from the preparation reported by Merkel et al.27 In particular, Lamberti et al.34 demonstrated that the gas permeability of PDMS can vary by a factor of four when the prepolymer-to-curing-agent ratio is changed. Physically, this variation arises from alterations to the free-volume “holes” in the polymer matrix–a notion supported by earlier observations of Carrillo et al.35 and Stafie et al.,36 which highlight how increasing the crosslinker content reduces the size and number of these voids, thereby curbing gas transport. Consequently, even moderate shifts in PDMS preparation could readily explain the gap between our parameter a and the value inferred from Merkel's data. It is also worth noting that Merkel et al. purchased their PDMS membranes and do not provide quantitative details about the curing agent, hence it is probably illusory anyway to expect a 1
γ)−1 = 0.0105 μm−3 s. This value agrees in order of magnitude with our fitting value a = 0.024 μm−3 s, but it is two times lower. We shall discuss later some reasons for this discrepancy, in relation with some simplifying assumptions of the model. However, a probable explanation for this factor-of-two difference is the specific PDMS recipe used here, which differs from the preparation reported by Merkel et al.27 In particular, Lamberti et al.34 demonstrated that the gas permeability of PDMS can vary by a factor of four when the prepolymer-to-curing-agent ratio is changed. Physically, this variation arises from alterations to the free-volume “holes” in the polymer matrix–a notion supported by earlier observations of Carrillo et al.35 and Stafie et al.,36 which highlight how increasing the crosslinker content reduces the size and number of these voids, thereby curbing gas transport. Consequently, even moderate shifts in PDMS preparation could readily explain the gap between our parameter a and the value inferred from Merkel's data. It is also worth noting that Merkel et al. purchased their PDMS membranes and do not provide quantitative details about the curing agent, hence it is probably illusory anyway to expect a 1![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) :
:![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) 1 comparison between their reported solubilities and the ones inferred from our study.
1 comparison between their reported solubilities and the ones inferred from our study.
![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) is negative. We may then extend the conservation of air (2) simply by evaluating the width at the meniscus location:
 is negative. We may then extend the conservation of air (2) simply by evaluating the width at the meniscus location:| hw(x = L) ![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) = −Q, | (12) | 
|  | (13) | 
Once the profile w(x) is known, it is a simple matter to compute the remaining integral, and to insert the expression of Q into the equation of conservation of air (12) to obtain a (nonlinear) differential equation for the dynamics of the meniscus.
To test this idea experimentally, we designed two channels with linearly variable width (Fig. 2b). They are both of length Lc = 5.5 mm, and their width varies linearly between 80 and 225 μm, one with increasing width, and the other with decreasing width; hence, they contain the same volume. We plot in Fig. 7a the time evolution of the length of the gas pocket for this two channels. Interestingly, whilst this length decreases initially faster in the channel with increasing width, there is a crossover at t = 4 × 103 s in Fig. 7a, and eventually the gas pocket disappears first in the channel with decreasing width. Moreover, the shape of the curves is no longer exponential as it was for channels of uniform width (Fig. 3). Indeed, plotting |![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) | as a function of L shows that whilst we get straight lines for channels of uniform width, we get a convex curve for the channel of increasing width, and a concave curve for the channel of decreasing width (Fig. 7b).
| as a function of L shows that whilst we get straight lines for channels of uniform width, we get a convex curve for the channel of increasing width, and a concave curve for the channel of decreasing width (Fig. 7b).
|  | ||
| Fig. 7  (a) Time evolution of the length of the air-filled part of two channels, one of increasing width (◁) and one of decreasing width (▷). The recording for this experiment has been stopped at 7000 s. (b) Corresponding plot of the velocity of the air/liquid interface as a function of the length of the air-filled part; curves are fits by eqn (14). The inset zooms in the region of low values of L and | ![[L with combining dot above]](https://www.rsc.org/images/entities/i_char_004c_0307.gif) |. | ||
To capture the experimental results, we use the following expression for the width varying linearly between w1 at the close end (x = 0) and w0 at the open end (x = Lc): w(x) = w1 + (w0 – w1)x/Lc. Inserting this expression in (13) and using (12), we get the following differential equation:
|  | (14) | 
![[L with combining macron]](https://www.rsc.org/images/entities/i_char_004c_0304.gif) = L/Lc,
 = L/Lc, ![[w with combining macron]](https://www.rsc.org/images/entities/i_char_0077_0304.gif) = w0/w1 and
 = w0/w1 and ![[h with combining macron]](https://www.rsc.org/images/entities/i_char_0068_0304.gif) = h/w1. This is a separable equation which can be solved analytically to yield an implicit solution of the form t(
 = h/w1. This is a separable equation which can be solved analytically to yield an implicit solution of the form t(![[L with combining macron]](https://www.rsc.org/images/entities/i_char_004c_0304.gif) ), but this is a tedious task, and it is much more direct to fit the data from Fig. 7b with the right-hand side of (14), with a as a free fitting parameter. The fitting curve is in excellent agreement with the data. This validates the extension of our analysis of imbibition for channels of varying width.
), but this is a tedious task, and it is much more direct to fit the data from Fig. 7b with the right-hand side of (14), with a as a free fitting parameter. The fitting curve is in excellent agreement with the data. This validates the extension of our analysis of imbibition for channels of varying width.
    
    
      
      Moreover, the channel may deform and bulge out because the gas pocket is capillary overpressure pin − p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) with respect to the atmosphere. To get an estimate of this deformation, we proceed as in,43 and assume that the PDMS layer between the channel top and the atmosphere behaves as a thin elastic plate. Even though this layer is not slender in our experimental conditions, because δ is not much smaller than w, this should give the correct order of magnitude of its deflection. The latter is maximal at the centre of the channel, where it equals:44ζmax = (pin − p
 with respect to the atmosphere. To get an estimate of this deformation, we proceed as in,43 and assume that the PDMS layer between the channel top and the atmosphere behaves as a thin elastic plate. Even though this layer is not slender in our experimental conditions, because δ is not much smaller than w, this should give the correct order of magnitude of its deflection. The latter is maximal at the centre of the channel, where it equals:44ζmax = (pin − p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) )w4/ (384B), with a bending modulus B = Eδ3/[12(1 – ν2)] with E = 2 MPa the Young modulus of PDMS, and v = 0.5 its Poisson ratio. For the typical height h = 60 μm of our channels and their largest width (for which the deflection is maximal) w = 140 μm, and the expression (9) of the capillary pressure, we get the numerical evaluation: ζmax = 24 nm, which is negligible in comparison with the channel height. Even for the channel of smallest height h = 11 μm (the left point in Fig. 5c), for which w = 100 μm, we get ζax = 26 nm, which remains negligible. Therefore, the channel deformation can be safely neglected in our study.
)w4/ (384B), with a bending modulus B = Eδ3/[12(1 – ν2)] with E = 2 MPa the Young modulus of PDMS, and v = 0.5 its Poisson ratio. For the typical height h = 60 μm of our channels and their largest width (for which the deflection is maximal) w = 140 μm, and the expression (9) of the capillary pressure, we get the numerical evaluation: ζmax = 24 nm, which is negligible in comparison with the channel height. Even for the channel of smallest height h = 11 μm (the left point in Fig. 5c), for which w = 100 μm, we get ζax = 26 nm, which remains negligible. Therefore, the channel deformation can be safely neglected in our study.
![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) exceeding ambient pressure. In such a setup, operators normally stop or block other flows: the outlet, if present, is either sealed or set to the same pressure as the inlet. The gas pocket therefore remains stationary, whilst its internal pressure pin becomes:
 exceeding ambient pressure. In such a setup, operators normally stop or block other flows: the outlet, if present, is either sealed or set to the same pressure as the inlet. The gas pocket therefore remains stationary, whilst its internal pressure pin becomes:| pin = p ![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) + pcap, | (15) | 
![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) . Retaining the same treatment of the net diffusion flux through the channel walls, we obtain a generic expression for the characteristic timescale of bubble elimination:
. Retaining the same treatment of the net diffusion flux through the channel walls, we obtain a generic expression for the characteristic timescale of bubble elimination:|  | (16) | 
![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) the air solubility. The term penv is the external (often atmospheric) pressure, which can be made down to very low values by operators using vacuum to boost bubble removal. The term Γ(δ, w, h) encapsulates geometric factors dictating the overall permeation flux, as derived in a previous article related to pervaporation:21
 the air solubility. The term penv is the external (often atmospheric) pressure, which can be made down to very low values by operators using vacuum to boost bubble removal. The term Γ(δ, w, h) encapsulates geometric factors dictating the overall permeation flux, as derived in a previous article related to pervaporation:21|  | (17) | 
From an experimental standpoint, the parameter not always tabulated is the product D![[S with combining macron]](https://www.rsc.org/images/entities/i_char_0053_0304.gif) which can differ significantly based on fabrication factors – such as curing-agent ratio or post-baking steps – especially for elastomers like PDMS (see our discussion at the end of sec. 5). Once a single calibration experiment is performed for a given material (and preparation recipe), operators can extract this product, then apply eqn (16) to predict bubble-removal timescales under new geometric or pressure conditions.
 which can differ significantly based on fabrication factors – such as curing-agent ratio or post-baking steps – especially for elastomers like PDMS (see our discussion at the end of sec. 5). Once a single calibration experiment is performed for a given material (and preparation recipe), operators can extract this product, then apply eqn (16) to predict bubble-removal timescales under new geometric or pressure conditions.
Although eqn (16) was derived assuming uniform-width channels, an analogous treatment can be extended to more complex geometries like those in sec. 6, or even intricate network topologies. Moreover, whilst our derivation focused on PDMS due to its wide usage and high gas permeability, the same conceptual approach can be extended to other chip materials so long as their air-diffusion and solubility properties are known or can be calibrated. This versatility makes the overall framework broadly applicable to a range of bubble-management challenges in microfluidic devices.
Future explorations would profit from extending our approach to complex network architectures, such as branched and interconnected microfluidic layouts in which individual branches can compete or couple, making bubble removal more intricate. Another promising direction involves incorporating the deformability of soft channels, where elastocapillary effects become significant and channel walls can distend in response to local capillary pressures, potentially leading to unexpected dynamics. Furthermore, introducing strong geometric constrictions, as opposed to the incremental width variations explored here (sec. 6), may produce sharply nonlinear imbibition scenarios, much like what could be observed in the reverse configuration of air penetration in liquid-filled channels with constrictions.43 Indeed, such constrictions parallel the functionality of bordered pits in plant xylem,9,45,46 so investigating their influence in PDMS microchannels could provide fresh insights relevant to both biomimetic design and microfluidic applications.
![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) in the channel bounded by PDMS at the top, left and right edges (contact angle θ) and by glass at the bottom edge (contact angle θ′). Crucially, we assume that the contact angles are low enough that wedge-like gutters form ahead of the meniscus,47 as shown in the sketch of the cross section of the channel in Fig. 8. The success of our method relies on this assumption: as we shall see, it enables to bypass the direct computation of the meniscus curvature which can be done only numerically. For simplicity, we shall reason on a half-width of the cross section, without loss of generality.
 in the channel bounded by PDMS at the top, left and right edges (contact angle θ) and by glass at the bottom edge (contact angle θ′). Crucially, we assume that the contact angles are low enough that wedge-like gutters form ahead of the meniscus,47 as shown in the sketch of the cross section of the channel in Fig. 8. The success of our method relies on this assumption: as we shall see, it enables to bypass the direct computation of the meniscus curvature which can be done only numerically. For simplicity, we shall reason on a half-width of the cross section, without loss of generality.
      On Fig. 8, we denote ![[scr A, script letter A]](https://www.rsc.org/images/entities/char_e520.gif) the area filled with air, which spans the cross section excluding the gutters. The outer perimeter
 the area filled with air, which spans the cross section excluding the gutters. The outer perimeter ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) of this air-filled region is split in three parts:
 of this air-filled region is split in three parts: ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) =
 = ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) L +
L + ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) P +
P + ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) g, where
g, where ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) L is the perimeter between air and liquid,
L is the perimeter between air and liquid, ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) P the perimeter between the air and PDMS, and
P the perimeter between the air and PDMS, and ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) g the perimeter between the air and glass. Considering a virtual displacement dx of the meniscus in the longitudinal direction of the channel yields the following virtual work balance: (pin − p
g the perimeter between the air and glass. Considering a virtual displacement dx of the meniscus in the longitudinal direction of the channel yields the following virtual work balance: (pin − p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) )
)![[scr A, script letter A]](https://www.rsc.org/images/entities/char_e520.gif) dx = γ(
dx = γ(![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) L +
L + ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) P
P![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) cos
cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ +
θ + ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) g
g![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) cos
cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ′)dx. This equation is a straightforward extension of the approach of Mason and Morrow,30 who considered a single contact angle, to the case of two contact lines on two solid materials with different contact angles. The capillary pressure is related to the mean radius of curvature r of the meniscus by pin − p
θ′)dx. This equation is a straightforward extension of the approach of Mason and Morrow,30 who considered a single contact angle, to the case of two contact lines on two solid materials with different contact angles. The capillary pressure is related to the mean radius of curvature r of the meniscus by pin − p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) = γ/r; and r is also the radius of curvature of the gutters far ahead the meniscus, as their cross section becomes independent of x. Hence, r obeys the relation:
 = γ/r; and r is also the radius of curvature of the gutters far ahead the meniscus, as their cross section becomes independent of x. Hence, r obeys the relation:
|  | (18) | 
We now consider the geometry of the gutters, to transform (18) into a equation of the second degree relating r to h, w, θ and θ′. First, ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) L is the curvilinear length of the two arcs of circle AB and A′B′:
L is the curvilinear length of the two arcs of circle AB and A′B′:
| ![[scr P, script letter P]](https://www.rsc.org/images/entities/char_e52f.gif) L = r(π − 3θ −θ′). | (19) | 
Then, from elementary geometry, O′D′ = r![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) cos
cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ, D′A′ = r
θ, D′A′ = r![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) sin
sin![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ, O′E′ = r
θ, O′E′ = r![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) cos
cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ′ and E′B′ = r
θ′ and E′B′ = r![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) sin
sin![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ′. Hence, B′C′ = E′C′ − E′B′ = O′D′ − E′B′ = r(cos
θ′. Hence, B′C′ = E′C′ − E′B′ = O′D′ − E′B′ = r(cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ − sin
θ − sin![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ′). Since B′C′ must be positive for a gutter to form, a necessary condition for the existence of a gutter at the corner between PDMS and glass is therefore cos
θ′). Since B′C′ must be positive for a gutter to form, a necessary condition for the existence of a gutter at the corner between PDMS and glass is therefore cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ > sin
θ > sin![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ′. We thus obtain:
θ′. We thus obtain:
|  | (20) | 
We also have A′C′ = O′E′ − A′D′ = r(cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ − sin
θ − sin![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ′). Similarly, we obtain OD = OE = r
θ′). Similarly, we obtain OD = OE = r![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) cos
cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ, and DA = EB = r
θ, and DA = EB = r![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) sin
sin![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ, hence AC = BC = r(cos
θ, hence AC = BC = r(cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ − sin
θ − sin![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ), which shows that a necessary condition for the existence of a gutter at the corner between two PDMS sides is θ < π/4, as already known.47 Hence,
θ), which shows that a necessary condition for the existence of a gutter at the corner between two PDMS sides is θ < π/4, as already known.47 Hence,  . Moreover, A′B′ = h – BC − A′C′ = h – r(cos
. Moreover, A′B′ = h – BC − A′C′ = h – r(cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ + cos
θ + cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ′ − 2
θ′ − 2![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) sin
sin![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ). We can thus express the perimeter between air and PDMS:
θ). We can thus express the perimeter between air and PDMS:
|  | (21) | 
Finally,  . Now, from elementary geometry,
. Now, from elementary geometry,  . Similarly,
. Similarly,  . Hence,
. Hence, 
|  | (22) | 
Inserting (19)–(22) in (18), and simplifying after some algebra, yields the equation of second degree for the gutter curvature κ = 1/r:
|  | (23) | 
|  | (24) | 
 , which is obviously positive in the relevant range 0 ≤ θ < π/4 for the contact angle. Hence, there are two real solutions κ±, and a quick study of the signs of the coefficients of (24) show that the two solutions are positive, hence more work is required to determine which one gives the true curvature. However, for a positive solution to be physically admissible, two adjacent gutters must not merge, which requires A′B > 0 on Fig. 8. Hence, from the previous geometrical calculations, this sets a lower bound for the curvature: κ ≥ κc = (1 + cos
, which is obviously positive in the relevant range 0 ≤ θ < π/4 for the contact angle. Hence, there are two real solutions κ±, and a quick study of the signs of the coefficients of (24) show that the two solutions are positive, hence more work is required to determine which one gives the true curvature. However, for a positive solution to be physically admissible, two adjacent gutters must not merge, which requires A′B > 0 on Fig. 8. Hence, from the previous geometrical calculations, this sets a lower bound for the curvature: κ ≥ κc = (1 + cos![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ – 2
θ – 2![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) sin
sin![[thin space (1/6-em)]](https://www.rsc.org/images/entities/char_2009.gif) θ)/h. A quick calculation yields
θ)/h. A quick calculation yields  , which is obviously negative. But f(κ) defined in (24) is a second-order polynomial whose coefficient of order 2 is positive, hence κc lies between its two roots: κ− < κc < κ+, which proves that the only admissible curvature is:
, which is obviously negative. But f(κ) defined in (24) is a second-order polynomial whose coefficient of order 2 is positive, hence κc lies between its two roots: κ− < κc < κ+, which proves that the only admissible curvature is:![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) = γκ+ used in the main text in section 4.
 = γκ+ used in the main text in section 4.
      
      
         from eqn (23). Keeping only the largest root as the correct physical curvature, one gets:
 from eqn (23). Keeping only the largest root as the correct physical curvature, one gets:|  | (25) | 
This expression for the curvature can be taken directly to deduce the value of ΔPcap = pin − p![[small script l]](https://www.rsc.org/images/entities/char_e146.gif) = γκ+ in the final discussion (sec. 7) when discussing the generic expression to be used by microfluidic operators.
 = γκ+ in the final discussion (sec. 7) when discussing the generic expression to be used by microfluidic operators.
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